Appendix A. Covariant Vector Equation of Motion
This appendix transforms the linearized equation of motion of general relativity to a form identical to the covariant Lorentz force equation of electromagnetism.
The Lagrangian of a test mass in a weak external gravitational field is
,(A.1)
where the metric tensor has been linearized as ; is the Minkowski metric tensor of flat spacetime; is the velocity 4-vector of the test mass; is the Lorentz factor; and is the proper time interval. The linear approximation neglects all terms of order , including interactions of source masses with their own fields and with their own radiation, and including terms of order times test-mass acceleration.
The Euler-Lagrange equation is
.(A.2)
The equation of motion of a test mass in a weak external field, from (A.1) and (A.2), is
,(A.3)
where partial derivatives are indicated by .
A constant of motion for the test mass, , is found from (A.3) by
.(A.4)
The equation of motion of the test mass, from (A.3), is
.(A.5)
The equation of motion in terms of , from (A.5), is
,(A.6)
in which negligible terms of order have been added to the right-hand side.
The equation of motion in terms of and , from (A.6), is
.(A.7)
Appendix B. Covariant Vector Gravitational Field Equation
This appendix transforms the linearized field equation of general relativity to a vector field equation in a form identical to the covariant Maxwell equations of electromagnetism, and derives the general solution of the field equation for a point-mass source.
The transformation to a perturbation metric
that satisfies the Hilbert gauge condition,
, from Ref. [
3], is
and ,(B.1)
where and are the traces of and , respectively.
The field equation in terms of for the Hilbert gauge condition, , is
,(B.2)
where
is the gravitational constant and
is the energy-momentum tensor, from Ref. [
3].
The field equation in terms of , from (B.1) and (B.2), is
,(B.3)
where is the trace of .
The field equation in terms of the mass current-density 4-vector , from (B.3), is
.(B.4)
The solution of (B.4) through invariant Green functions, from Ref. [
22], is
,(B.5)
where is the range from source to test mass and is the delta function at the retarded time .
The conservation law, using , from (B.4), is
.(B.6)
The Hilbert gauge condition, , in terms of , from (B.3), is
.(B.7)
The field equation for a particle with energy-momentum tensor, , from (B.3), is
,(B.8)
where is the rest-mass density of the point mass ; is its velocity 4-vector; is its Lorentz factor; is its velocity 3-vector divided by the speed of light. For this point-mass source, the current density in the linear approximation is , where . The velocity 4-vector of the particle source and the velocity 4-vector of the test mass are coupled in the velocity 4-vector as a necessary step in the transformation of the equation of motion from a tensor equation to a covariant vector equation.
Appendix C. Gravimagnetic and Relativistic Gravitational Forces
This appendix derives the linearized (weak-field) equation of motion for two special cases: (i) Slow source with a slow test mass; and (ii) relativistic source with a stationary test mass.
The exact linearized space components of the equation of motion, from (A.3), are
,(C.1)
for . Equation (C.1) is derived from (A.3) by ranging the index separately over 0 and .
The linearized space components of the equation of motion of a relativistic test mass in the field of a slow source, , from (C.1), are
(C.2)
for .
The linearized space components of the equation of motion of a slow source, , with a slow test mass, and , from (C.2), are
,(C.3)
for . The first term on the right-hand side is the Newtonian force, and the anti-symmetric terms resemble a gravimagnetic force.
The linearized space components of the force of a relativistic source on a stationary test mass, and , from (C.1), are
,(C.4)
for .
In
Appendix G, the acceleration field of a point-source mass in the source-free radiation zone and in the transverse gauge will be derived from (C.4) through a different means than is used to derive the velocity field in
Appendix D. For the purpose of deriving the velocity field in
Appendix D, the perturbation metric of a relativistic source of mass density
with 4-velocity
may be represented, from (B.1), (B.2), and (B.8), as
,(C.5)
where the scalar quantity is a retarded Lorentz-transformed range from source to test mass; ; is a unit vector pointing from source to test mass; and all quantities within the brackets are evaluated at the retarded time .
The gravitational force in 3-vector notation of a relativistic point source of mass on a stationary test mass , to be used for calculating the velocity field, from (C.4) and (C.5), is
,(C.6)
where .
For comparison with (C.6), the electric force in 3-vector notation of a relativistic source of charge
on a stationary test mass
of charge
, from Ref. [
22], is
.(C.7)
Appendix D. Velocity Field of Relativistic Particles
This appendix derives the relativistically exact gravitational velocity field in the linear (weak-field) approximation. The derivation closely follows the derivation and nomenclature of the electric and magnetic velocity field from Ref. [
22].
From Ref. [
22], the equations used to derive the velocity field of a relativistic particle from (C.6) are
(D.1)
where ; is a unit vector pointing from source to test mass; is the retarded time; and an overdot indicates a derivative with respect to .
The gravitational field,
, in 3-vector notation of a relativistic source of mass
at a stationary test mass, from (C.6) and (D.1) and Ref. [
24], is
,(D.2)
where ; and is the derivative of the delta function with respect to its argument.
The electric field,
, in 3-vector notation of a relativistic source of charge
on a stationary test mass, corresponding to (D.2), from (C.7), (D.1), and Ref. [
22], is
.(D.3)
Changing the variable of integration in (D.2) to
, as in Refs. [
22] and [
24], and integrating by parts on the derivative of the delta function, gives the gravitational field at a stationary test mass, from (D.2), as
.(D.4)
The electric field, corresponding to (D.4), from Ref. [
22], is
.(D.5)
Using (D.1) to evaluate the time derivatives in (D.4), as in Ref. [
24], gives the relativistically exact (weak) retarded gravitational field of a source mass
with velocity
on a test mass instantaneously at rest at the spacetime point
as
,(D.6)
where an overdot indicates a derivative with respect to retarded time, as in .
The gravitational field in (D.6),
, comprises a velocity field
and an acceleration field
. Just as in electromagnetism, Ref. [
22], the velocity field is independent of the acceleration of the source mass and falls off with distance as
. The acceleration field depends linearly on acceleration and falls off as
.
In the source region or for a particle in uniform motion, , and the gravitational field is just the velocity field,
.(D.7)
The electric velocity field, corresponding to (D.7), from Ref. [
22], is
.(D.8)
To first order in , the Lorentz factor is , and the gravitational velocity field on a test mass at rest, from (D.7), is
.(D.9)
Hilbert repulsion, Refs. [
15,
16], appears in (D.7), but does not appear to first order in
in (D.9), because it only occurs for source speeds above
.
To first order in , the electric velocity field, from (D.8), is
,(D.10)
which has the same form as the gravitational velocity field in (D.9). Of course, the electric velocity field of a charge in (D.8) does not change sign at any velocity.
For a radially incoming particle of mass and uniform velocity, , , and the gravitational velocity field on a test mass at rest, from (D.7) is
,(D.11)
where is the range of the particle at the retarded time that the field was created, not the time that the field was detected. The gravitational field of the radially incoming particle becomes repulsive at source speeds above .
For a radially outgoing particle of mass and uniform velocity, , , and the gravitational velocity field on a test mass at rest, from (D.7) is
.(D.12)
The gravitational field of the outgoing particle also becomes repulsive at source speeds above .
The coordinate transformations from retarded (primed) coordinates
to isotropic (present) coordinates
for particles in uniform motion are given in Ref. [
15]. In terms of
, the field of the radially incoming particle in (D.11) is larger than the field of the outgoing particle in (D.12) by a factor
. But these are the fields at the range
of the particle at the retarded time
of production of the field, not at the range
of the particle at the present time
of detection of the field. In terms of the range
of the particle at the present time
, the fields in (D.11) and (D.12) are the same,
,(D.13)
for both radially incoming and outgoing particles.
For both radially incoming and outgoing ultrarelativistic particles of uniform velocity, , , and the repulsive gravitational velocity field on a test mass at rest in isotropic (present) coordinates, from (D.13) is
.(D.14)
Appendix E. Gravitational Impulse of a Particle in Uniform Motion
Figure 12 shows a configuration for calculating the gravitational impulse delivered to a test mass by a particle in uniform motion with constant momentum in the direction. Retarded (apparent) coordinates are primed; present isotropic coordinates, , are unprimed. The closest approach to the test mass occurs at , a distance from the test mass.
Figure A1.
Present and retarded positions of particle in uniform motion.
Figure A1.
Present and retarded positions of particle in uniform motion.
The nonzero metric components of a source in uniform motion, in retarded coordinates, from Refs. [
14,
15], (C.5), and Fig. E.1, are
,(E.1)
where is the trace of ; the scalar quantity is a retarded Lorentz-transformed range from source mass to test mass; and .
The velocity field of a particle in uniform motion, in retarded coordinates, from (D.6), is
.(E.2)
In electromagnetism, the electric velocity field of a charged particle in uniform motion, from (D.8), corresponding to (E.2), is
.(E.3)
Notice that the Hilbert repulsion term proportional to in the gravitational velocity field in (E.2) is not present in the electric velocity field in (E.3).
With reference to Fig. E.1, the transformation from retarded coordinates, , to present isotropic coordinates for a particle in uniform motion is derived from and , which together imply
and .(E.4)
The transformation from present to retarded coordinates, from Ref. [
15] and Fig. E.1, is
and .(E.5)
The inverse transformation from retarded to present coordinates, from Ref. [
15] and Fig. E.1, is
and .(E.6)
The transformation from retarded coordinates to present isotropic coordinates,
, leaves the scalar range to a test mass
m unchanged as
, where
and
, as in Refs. [
14,
15].
The velocity field in terms of present position, from (E.2) through (E.6) and Ref. [
15], is
.(E.7)
This equation predicts gravitational repulsion in present coordinates of a stationary test mass within a forward and backward cone for relativistic source speeds,
, corresponding to gravitational repulsion in retarded coordinates from (D.6) and Ref. [
15].
In electromagnetism, the electric velocity field in terms of present position, from (E.3) through (E.6) and Ref. [
15], corresponding to (E.7), is
.(E.8)
The transverse specific impulse delivered to a test mass by a particle in uniform motion with impact parameter , from (E.7), is
.(E.9)
Since the transverse impulse, , delivered to a test mass is equal and opposite to the impulse delivered to the particle, the angular deflection of the particle in the weak field of the test mass , for , from (E.9), is
.(E.10)
Appendix F. Quadrupole Radiation from a Rotating Binary
This appendix reviews the common derivation of quadrupole gravitational waves produced by a rotating binary, as presented, for example, in Refs. [
1,
2,
3,
4]. The interpretation of these waves is that they carry energy and momentum, but do not accelerate masses. Instead, these waves are believed to be curvature ripples on a flat spacetime background that cause coordinates to oscillate past masses, but do not cause the masses themselves to accelerate.
In
Appendix H, these quadrupole gravitational waves will be shown to be a linear superposition of dipole waves. Owing to a Doppler modulation effect, the dipole waves from each of the masses of a binary do not completely interfere. The superposition of the dipole waves from each of the masses has the same metric and same angular power distribution as the quadrupole wave from the binary, but the dipole waves do accelerate masses in accordance with the force equation.
The exact solution of the linearized field equation (B.2), from (C.5), is
,(F.1)
where the scalar quantity is a retarded Lorentz-transformed range from source to test mass; is the range from source to test mass; ; is a unit vector pointing from source to test mass; and all quantities within the brackets are evaluated at the retarded time .
The approximate solution in the radiation zone of (B.2) for a nonrelativistic source for which and and , from (F.1), is
.(F.2)
The space and time components of the Hilbert gauge condition with the conservation law , for , are
and .(F.3)
Evaluation of integrals in (F.2), from (F.3) and Ref. [
3], gives
.(F.4)
The proof of (F.4) by integration by parts and from (F.3) is
.(F.5)
Evaluation of integrals in (F.4), from (F.3) and Ref. [
3], gives
.(F.6)
The proof of (F.6) by integration by parts and from (F.3) is
.(F.7)
Combining (F.4) and (F.6) gives
.(F.8)
Combining (F.2) and (F.8) gives
.(F.9)
To zeroth order in , , and (F.9) is approximately given by
,(F.10)
where is the second derivative with respect to the retarded time of the quadrupole moment; if ; and if . Since the term proportional to does not carry energy, it is omitted from (F.10) and from the calculation of energy flux.
Figure 1 in Sec. 3.1 shows a configuration for calculating the quadrupole radiation of a binary system comprising two particles of masses
and
moving in circular orbits with constant angular frequency
and constant speeds
and
, respectively, about their center of mass.
The retarded coordinates of and , respectively, from Fig. 1, are
,(F.11)
where and are the constant orbital radii of and , respectively.
The only nonzero components , from (F.10) and (F.11), are
,(F.12)
where is the reduced mass of the binary, and is the distance between the masses.
The only nonzero linearized fields for , from (F.10) and (F.12), are
,(F.13)
where .
The partial time derivatives of the fields, since is nearly constant, from (F.13), are
.(F.14)
The only dependence of on , since is nearly constant, is in the retarded time , so that
,(F.15)
where is the constant radial unit vector in spherical coordinates; and , , and are directional unit vectors at the source.
Using (F.15), the Hilbert gauge condition, , gives
.(F.16)
From (F.14), (F.16) becomes
.(F.17)
The energy-momentum tensor
associated with a free gravitational field, from Ref. [
3], is given by
.(F.18)
The energy flux of radiation in the radial direction, , for, , , from (F.14), (F.17), and (F.18), is given by
.(F.19)
The energy per unit time per unit solid angle radiated in the radial direction , from (F.19), is
.(F.20)
The total quadrupole power radiated from the rotating binary shown in Fig. 1, from (F.20), is
.(F.21)
Appendix G. Acceleration Field of Relativistic Particles
This appendix derives the exact gravitational acceleration field of a relativistic particle in the radiation zone for . The derivation from the tensor “potential” differs somewhat
from the derivation of the electric acceleration field from the electric vector potential
in Ref. [
22].
In the source-free radiation zone, in the transverse (Coulomb) gauge. The k-component, , of the gravitational field of a relativistic particle at a stationary test mass in the radiation zone, therefore, from (C.4), is
.(G.1)
The perturbation-metric component in the radiation zone of a relativistic particle with 4-velocity , from (C.5), is
,(G.2)
where the scalar quantity is a retarded Lorentz-transformed range from source to test mass; is the range from the source at to the test mass at ; ; is a unit vector pointing from source to test mass; and all quantities within the brackets are evaluated at the retarded time .
For a particle with mass density , in the integral in (G.2) cannot simply be replaced by in the radiation zone. Instead, similar to (F.4) and (F.6),
.(G.3)
The proof of (G.3) from integration by parts and from the time component of the conservation law, , in the source-free radiation zone, similar to the proofs (F.5) and (F.7), is
.(G.4)
In the radiation zone, the range
from source to test mass is approximately constant for a test mass at rest, because
. As in
Appendix D, for simplicity from this point forward,
and
are taken to be constants, as they are, for example, for a particle moving at constant speed in a circular orbit.
The perturbation-metric components in the radiation zone, from (G.2) and (G.3), are
,(G.5)
where is the k-component, , of the dipole moment of a particle of mass .
Appendix H. Dipole Radiation from a Rotating Binary
This appendix derives the angular power distribution of gravitational radiation and the total power radiated by a rotating binary in a manner entirely different from the common derivation reviewed in
Appendix F.
This appendix shows that a quadrupole gravitational wave radiated by a rotating binary is actually a linear superposition of dipole waves from each of the masses. Owing to a Doppler modulation effect, the dipole waves from each of the masses of a binary do not completely interfere. The superposition of the dipole waves from each of the masses of a binary has the same metric and same angular power distribution as was derived in
Appendix F for a quadrupole wave. But the dipole waves accelerate masses in accordance with the force equation of
Appendix C, and do not merely produce curvature ripples on a flat spacetime background.
The perturbation-metric components , , in the radiation zone of a binary, from (G.5), are
,(H.1)
where the scalar quantity is a retarded Lorentz-transformed range from source mass to test mass; is the nearly constant range from the source at to the test mass at ; ; is a unit vector pointing from source to test mass; and all quantities within the brackets are evaluated at the retarded time .
The perturbation-metric components , , in the radiation zone of the rotating binary system of particles with masses and shown in Fig. 1, from (G.5) and (H.1), are
,(H.2)
where and are the k-components of the dipole moments; and are the Doppler factors; and are the 4-velocities; and and are the constant Lorentz factors of and .
The coordinates and velocities of and for the binary shown in Fig. 1, from (F.11), are
,(H.3)
where is the constant unit vector in the direction from source to test mass; and are the constant polar and azimuthal angles of the test mass in spherical coordinates; and are the constant orbital radii of and ; and and .
Since the momenta of the masses are equal and opposite and are first order in , to first order in the dipole components of the binary are zero. To second order in , the nonzero dipole components , from (H.2) and (H.3), are
,(H.4)
where ; is the reduced mass of the binary; and is the distance between the masses.
Since is about constant in the radiation zone, the derivative is replaced in (H.4) by because
.(H.5)
Since the components of the dipole wave interference pattern in (H.4) , calculated as a superposition of dipole waves from each mass of a binary, are identical to the components of the quadrupole wave pattern in (F.17), by the Hilbert gauge condition, all the other components of are identical as well. That is, by the Hilbert gauge condition, from (F.14), (F.17), and (H.4), the components are
.(H.6)
Since all the components
of the dipole wave interference pattern are identical to the components
of the quadrupole wave pattern of
Appendix F, the dipole energy
per unit time per unit solid angle
radiated in the radial direction, from (F.20),
,(H.7)
and the total dipole power radiated from the rotating binary shown in Fig. 1, from (F.21),
,(H.8)
are identical as well.
The difference between the dipole wave interference field, as derived in (H.4) and (H.6), and the quadrupole wave field, as derived in (F.14) and (F.17), is that the dipole field accelerates mass in the radiation zone in accordance with the equation of motion, as seen in App. I.
Appendix I. Dipole Vector Gravitational Field of a Rotating Binary
This appendix derives the dipole gravitational acceleration field in the transverse gauge of the rotating binary shown in Fig. 1 at a stationary test mass in the radiation zone.
In accordance with the equation of motion, (C.4), the acceleration of a test mass at rest at in the source-free radiation zone, by the rotating binary system of particles with masses and shown in Fig. 1, is the dipole vector gravitational acceleration field in the transverse gauge, which from (C.4) and (H.4) is
,(I.1)
where the nomenclature is the same as in
Appendix H and
.(I.2)
The dipole field in the radiation zone, from (I.1) and (I.2), is
.(I.3)
By cylindrical symmetry, the field is independent of azimuthal angle . In particular, for , the dipole field in the radiation zone, in the x-z plane of the binary, from (I.3), is
.(I.4)
The transformation from the basis at the binary to the basis at the test mass, where is the direction of propagation of the dipole wave, and as in (I.4), is
.(I.5)
The dipole field propagating in the direction in the transverse gauge at the test mass in the radiation zone, from (I.4) and (I.5), is
.(I.6)
The dipole vector gravitational field (I.6) is the plane-wave vector-field solution of the covariant-vector gravitational field equation (B.8) for slow velocities of the binary shown in Fig. 1 and for the special case in (C.6) of a test mass at rest in the radiation zone.
Appendix J. The Polarization and Power of Vector Gravitational Plane Waves
This appendix is a general treatment of the polarization and power of dipole vector-field plane-wave solutions of the gravitational field equation in the slow-source linear approximation. The treatment is consistent with the common derivation of quadrupole tensor-field plane-wave solutions in the slow-source linear approximation, such as in App. F.
Even though dipole vector fields accelerate masses as in App. I, and do not merely produce curvature ripples on a flat spacetime background as in App. F, a gravitational-wave detector makes no distinction in the linear approximation, as was demonstrated in App. H. In the linear approximation, the perturbation metrics are identical. Nonlinear events, however, like those detected at gravitational-wave observatories, can produce dipole gravitational radiation at the orbital frequency, which is half the quadrupole frequency, as discussed in App. K.
Unit 4-vectors and a wavenumber 4-vector are defined for gravitational plane waves as
, , , , ,(J.1)
where is the angular frequency of the wave.
Transverse traceless polarization tensors are commonly defined for quadrupole gravitational plane waves with as
and .(J.2)
Transverse traceless polarization tensors are defined for dipole gravitational plane waves with as
and .(J.3)
The perturbation metric satisfying the Hilbert gauge condition for dipole gravitational waves in the radiation zone of the binary shown in Fig. 1, from Apps. F and H and (J.1), (J.2), and (J.3), is
,(J.4)
where .
In 3-vector notation, transverse polarization vectors of dipole gravitational plane waves having wavenumber 3-vector , where is a unit vector in the (radial) direction of propagation, are given by the unit 3-vectors,
and .(J.5)
Transverse dipole gravitational and gravimagnetic plane-wave vector fields at a test mass are of the form
,(J.6)
where and are complex amplitudes.
For the dipole vector field in (I.6), of the binary shown in Fig. 1, , and from (I.6) and (J.6),
,(J.7)
so that and in (J.6).
Circularly polarized dipole gravitational plane-wave fields, with positive and negative helicity respectively, are of the form
,(J.8)
where is a complex amplitude.
In the orbital plane, where , the dipole field in (J.7) is linearly polarized. As the test mass approaches the axis of rotation of the binary, where , the polarization approaches circular polarization, though the amplitude of the dipole wave vanishes on the axis, where .
The transverse dipole plane-wave vector fields represented by (J.6) have an instantaneous energy flux of a gravitational acceleration field at a stationary detector in the radiation zone,
,(J.9)
where is the gravimagnetic field.
Poynting’s vector, the instantaneous energy flux of an electromagnetic acceleration field at a stationary detector in the radiation zone, corresponding to (J.9), from Ref. [
22], is
,(J.10)
where is the magnetic acceleration field.
The electromagnetic power radiated by the source per unit solid angle, from (J.10), is
.(J.11)
The dipole gravitational power radiated by the source per unit solid angle, corresponding to (J.11), from (I.7) and (J.9), is
.(J.12)
The total dipole power radiated continuously by the rotating binary shown in Fig. 1, obtained by integrating over all solid angle, from (J.12), is
,(J.13)
in agreement with (F.21) and (H.8).
Appendix K. Dipole Radiation from an Isolated Mass Dipole
This appendix calculates the gravitational field and angular distribution of dipole radiation from an isolated accelerating mass dipole in general, and then the radiation for the specific example of a mass caused to move in a circular orbit, for example, by a continuous circularly polarized wave, such as an electromagnetic wave or a dipole gravitational wave.
The perturbation-metric components , , of an isolated mass in the radiation zone, from (G.5), are
,(K.1)
where the scalar quantity is a retarded Lorentz-transformed range from source to test mass; is the nearly constant range from the source at to the test mass at ; is the k-component of the dipole moment; is the Doppler factor; is a unit vector pointing from source to test mass; is the 4-velocity; is the constant Lorentz factor of ; and all quantities within the brackets are evaluated at the retarded time .
To first order in , the nonzero dipole components , from (H.4), (H.5), and (K.1), are
,(K.2)
where an overdot indicates a derivative with respect to the retarded time .
In accordance with the equation of motion, (C.4), the acceleration of a test mass at rest at in the source-free radiation zone, by the particle moving in accordance with (K.2), is the dipole vector gravitational acceleration field in the transverse gauge, from (C.4) and (K.2),
.(K.3)
To the same first order in
, the electric acceleration field in the transverse gauge of an isolated charge
acting on a test charge at rest at
in the source-free radiation zone, corresponding to (K.3), from Ref. [
22], is
.(K.4)
Poynting’s vector, the instantaneous energy flux of an electromagnetic acceleration field propagating in the
direction to a stationary detector in the radiation zone, from Ref. [
22], is
,(K.5)
where is the magnetic acceleration field.
The electromagnetic power radiated by the source per unit solid angle, from (K.5) and Ref. [
22], is
,(K.6)
where is the instantaneous angle between and .
The total instantaneous dipole power radiated by the charge
, from integrating (K.6) over all solid angle, is the familiar Larmor result for a nonrelativistic accelerated charge, from Ref. [
22],
,(K.7)
where is the second time derivative of the electric dipole moment .
The instantaneous energy flux of a gravitational acceleration field propagating in the direction to a stationary detector in the radiation zone, corresponding to (K.5), from (J.9), is
, (K.8)
where is the gravimagnetic field.
The dipole gravitational power radiated per unit solid angle by the isolated mass, corresponding to (K.6), from (K.3) and (K.8), is
(K.9)
where is the instantaneous angle between and .
The total instantaneous dipole power radiated into the radiation zone by the isolated nonrelativistic accelerated mass , corresponding to the familiar Larmor result in (K.7) for a nonrelativistic accelerated charge, from integrating (K.9) over all solid angle, is
,(K.10)
where is the second time derivative of the mass dipole moment .
The dipole gravitational field in (K.3) and the angular power distribution in (K.9) and total dipole power in (K.10) apply generally to any isolated nonrelativistic accelerated mass. As a specific example, the radiation by a mass caused to move at constant speed in a circular orbit by a continuous circularly polarized wave is now calculated.
The coordinates and velocity of an isolated mass moving in a circular orbit of radius and angular frequency are
,(K.11)
where is the constant unit vector in the direction from source to test mass; and are the constant polar and azimuthal angles of the test mass in spherical coordinates; and .
To first order in , the nonzero dipole components , from (K.2) and (K.11), are
.(K.12)
In accordance with the equation of motion, (C.4), the acceleration of a test mass at rest at in the source-free radiation zone, by the particle moving in accordance with (K.2), is the dipole vector gravitational acceleration field in the transverse gauge, from (C.4) and (K.3),
.(K.13)
The transformation from the basis at the binary to the basis at the test mass, where is the direction of propagation of the dipole wave, and , from (I.5), is
.(K.14)
The dipole field propagating in the direction in the transverse gauge at the test mass in the radiation zone, from (K.13) and (K.14), is
.(K.15)
The dipole vector gravitational field (K.15) is the plane-wave vector-field solution of the covariant vector gravitational field equation (B.8) for slow velocities of an isolated mass in constant circular motion and for the special case in (C.6) of a test mass at rest in the radiation zone.
The instantaneous energy flux of the dipole field at a stationary detector in the radiation zone, from (K.8) and (K.15), is
.(K.16)
The dipole gravitational power radiated per unit solid angle by the isolated mass, corresponding to (K.6), from (K.3) and (K.8), is
.(K.17)
The total dipole power radiated continuously by the isolated mass in constant circular motion, obtained by integrating over all solid angle, from (K.17), is
,(K.18)
in agreement with (K.10), and corresponding to the Larmor electromagnetic power formula in (K.7).
Appendix L. Strain Waveform Model for Merger Event GW150914
As shown in (H.4) and (I.6), the dipole gravitational waves from each of the masses of a well-behaved binary, produced at the orbital angular frequency , interfere almost completely. The resulting interference waveform has an angular frequency .
The events detected at gravitational wave observatories are generally mergers of massive compact binaries producing highly nonlinear fields in their source regions. The dipole waves from each of the masses are distorted and delayed by the strong gravitational fields of their companions. These nonlinear effects within the source region disturb the linear interference of the waveforms and leave a trace dipole signal at the orbital angular frequency . A detailed calculation of the dipole radiation at orbital frequency requires numerical relativity.
This appendix shows how a simple waveform model can be used to estimate the dipole radiation power at the orbital frequency produced nonlinearly by the specific merger event, GW150914.
Figure 2 in Sec. 3.4 shows the unfiltered gravitational-wave strain signal of event GW150914 observed by the LIGO Hanford detector. The waveform model focuses only on the eight strain amplitude peaks
,
, indicated by circles in Fig. 2(a) at
. (L.1)
The quartic-polynomial least-squares fit to these 8 data points,
,(L.2)
indicated by the dashed curve in Fig. 2(a), is considered the envelope of the quadrupole signal amplitude in the waveform model.
As the masses spiral inwards with successively shorter orbital periods, the frequency chirp is modeled by a linearly increasing frequency from each amplitude peak to the next, such that the amplitude peaks in the model occur at exactly the same time as those in the signal, indicated by circles in Fig. 2(a). This provides a continuous orbital angular frequency function for the model.
Figure 2(a) shows an alternating pattern of amplitude peaks above and below the dashed least-squares-fit curve, which suggests that a small dipole signal at orbital frequency
could be superposed on the main signal at
. The purpose of the strain waveform model is to estimate the order of magnitude of such a possible dipole signal relative to the main signal.
The dipole signal is modeled by a frequency equal to half the main wave frequency and by an amplitude envelope, , equal to the quadrupole amplitude envelope reduced by the constant fraction , which is a parameter in the model. The model of the strain waveform of the superposed quadrupole and dipole waves is
,(L.3)
where s is the time of the initial amplitude peak in Fig. 2.
As shown in Fig. 3, the variance between the model waveform and the actual strain waveform is a minimum for . That is, the model waveform best fits the peak amplitudes of the Hanford LIGO strain signal from the GW150914 event for a dipole signal amplitude at frequency equal to 7.2 percent of the main signal amplitude at . This amplitude corresponds to about 0.5 percent of the power radiated at the orbit frequency. The improvement in the matching of the model with the strain signal by including a superposed dipole signal at the orbit frequency and at amplitude ratio is seen by comparing Fig. 2(a) to 2(b).
Appendix M. Scattering of Dipole Gravitational Waves by a Free Particle
This appendix calculates the total scattering cross section for scattering of unpolarized dipole gravitational radiation by free particles, corresponding to the Thomson cross section for scattering of unpolarized electromagnetic radiation by free charges.
The equation of motion of a free particle of velocity , initially at rest in the radiation zone of an isolated accelerating mass with slow velocity (), in the transverse gauge, from (K.3) is
,(M.1)
where ; is the displacement vector from the retarded source position to the free particle at ; ; is unit vector pointing from the source to the particle; and brackets mean the quantity inside is evaluated at the retarded time .
The dipole gravitational field of a linearly polarized plane wave in the radiation zone produced by a source mass oscillating at angular frequency , from (M.1), is
,(M.2)
where is the wave amplitude; is a unit polarization 3-vector in the direction of , which is transverse to the wavenumber 3-vector .
The dipole gravimagnetic field corresponding to the dipole gravitational field in (M.2), from (K.8), is
.(M.3)
The dipole gravitational power radiated per unit solid angle from a free particle of mass , velocity , and acceleration , for , from (K.9), is
,(M.4)
where is the instantaneous angle between and , a unit vector in the direction of radiation from the free particle.
The time-averaged angular distribution of dipole power radiated from a free particle of mass in the field of a plane dipole gravitational wave , from (M.2) and (M.4), is
.(M.5)
The total dipole power radiated from a free particle, from (K.10), is
.(M.6)
The time-averaged total dipole power radiated from a free particle of mass in the field of the plane dipole gravitational wave , from (M.2) and (M.6), is
.(M.7)
The instantaneous energy flux of the plane dipole gravitational wave in the radiation zone, in the direction of propagation of , from (K.16), is
.(M.8)
The time-averaged energy flux in the direction of propagation of a plane dipole gravitational wave in the radiation zone, from (M.2) and (M.8), is
.(M.9)
The differential scattering cross section for scattering of a plane-polarized dipole gravitational wave by a free particle of mass , if the particle moves a negligible fraction of a wavelength over one oscillation cycle, from (M.5) and (M.9), is
.(M.10)
The differential scattering cross section for scattering of a plane-polarized electromagnetic wave by a particle of mass
and charge
, corresponding to (M.10), from Ref. [
22], is
.(M.11)
The dipole angular distribution
, from (K.17) and Ref. [
22], is
,(M.12)
where the wave is incident along the axis; the polarization vector makes an angle with the axis; and the direction of radiation is along a polar angle from the axis and an azimuthal angle from the axis.
The differential scattering cross section for scattering of unpolarized dipole gravitational radiation by a free particle of mass , from (M.10) and (M.12), by averaging over , is
.(M.13)
The Thomson formula for scattering of electromagnetic radiation by a free charge
, corresponding to (M.13), from Ref. [
22], is
.(M.14)
The total scattering cross section for scattering of unpolarized dipole gravitational radiation by a free particle of mass , from (M.13), is
.(M.15)
This cross section is valid only for frequencies at which quantum-mechanical effects are insignificant, that is, for , where is the reduced Planck constant.
The total electromagnetic scattering cross section, called the Thomson cross section, for scattering of
unpolarized electromagnetic radiation by a free charge
, corresponding to (M.15), from (M.14) and Ref. [
22], is
.(M.16)
The Thomson cross section is also valid only for frequencies .
Appendix N. Scattering of Dipole Gravitational Waves by a Mass Oscillator
This appendix calculates the total scattering cross section for scattering of unpolarized dipole gravitational radiation by oscillators at resonance, and the line width of dipole gravitational radiation from oscillators at resonance.
The equation of motion of a simple harmonic oscillator of resonant angular frequency and damping constant , driven by a dipole gravitational wave with constant amplitude and polarization in the direction, is
,(N.1)
where an overdot indicates a derivative with respect to time.
The solution of (N.1) is
, where .(N.2)
The kinetic energy of an oscillator of mass , driven by a dipole gravitational wave , from (N.2), is
,(N.3)
where is the total energy, kinetic plus potential, of the oscillator driven by a dipole gravitational wave of angular frequency .
The line width , defined as the full width at half-maximum (FWHM) energy, from (N.3), is
, (N.4)
where the quality factor is .
Driven at resonant frequency, , the oscillator kinetic energy, from (N.3) and (N.4), is
.(N.5)
Driven at resonant frequency, the oscillator speed and acceleration, from (N.3) and (N.5), are
.(N.6)
Driven at resonant frequency, the oscillator radiates a total dipole power in steady state, from (M.6) and (N.6),
.(N.7)
The time-averaged dipole power radiated from the oscillator at resonance in steady state, from (M.7) and (N.7), is
,(N.8)
where from (M.7) is the time-averaged dipole power radiated from a free particle driven by the same dipole gravitational wave .
The total scattering cross section for scattering of unpolarized dipole gravitational radiation by the oscillator at resonance, from (M.15) and (N.8), is
.(N.9)
The total energy, kinetic plus potential, of the oscillator at resonance, from (N.5), is
. (N.10)
The time-averaged fractional rate of energy radiated by the oscillator at resonance in steady state, from (N.8) and (N.10), is
,(N.11)
which is proportional to the “spring constant” of the oscillator.
From the solution of the homogeneous equation, , the time-averaged total energy of the oscillator at resonance after the driving force is suddenly removed at , from (N.10), is
.(N.12)
The time-averaged rate of fractional energy loss by radiation from the oscillator at resonance after the driving force is suddenly removed at , from (N.11) and (N.12), is
.(N.13)
The FWHM line width of dipole gravitational radiation from the oscillator of mass at resonant frequency , from (N.4) and (N.13), is
,(N.14)
which is proportional to the “spring constant” of the oscillator.
Appendix O. Quantization and Statistics of the Cosmic Gravitational Background (CGB)
This appendix calculates the properties of the CGB assuming it is a collection of spin-1 bosons in thermal equilibrium obeying photon statistics.
If the vector gravitational field of the CGB is regarded as quantized, then the associated spin-1 graviton is a relativistic particle with 4-momentum
,(O.1)
where is the wavenumber 4-vector, and is the reduced Planck constant.
If the CGB is a collection of indistinguishable, massless, spin-1 bosons obeying photon statistics and is in thermal equilibrium at absolute temperature , the mean number of bosons in each state is given by the Planck distribution,
,(O.2)
where is the energy of a boson in state , and is Boltzmann’s constant.
The mode density (number of modes per unit volume) per unit angular frequency for both directions of polarization is identical to that of the cosmic microwave background (CMB),
.(O.3)
The mean number density of spin-1 gravitons per unit angular frequency, in the frequency range from to , from (O.2) and (O.3), is
,(O.4)
where is the energy of a spin-1 graviton in the frequency range from to .
The mean total number density of spin-1 gravitons in all frequencies, found by integrating (O.4), is
,(O.5)
where is the Riemann zeta function (with argument 3).
The mean energy density of spin-1 gravitons per unit angular frequency, in the frequency range from to , from (O.4), is
.(O.6)
The mean energy density of gravitons per unit angular frequency, in (O.6), is a maximum at frequency , corresponding to wavelength , given by Wien’s displacement law,
.(O.7)
The mean total energy density in all frequencies, found by integrating (O.6), is the Stefan-Boltzmann law,
.(O.8)
The mean energy per spin-1 graviton, from (O.5) and (O.8), is
.(O.9)
Appendix P. Fluctuating Gravitational Fields of the CGB from Nyquist Relations
This appendix calculates the energy density of stochastic dipole gravitational fields in thermal equilibrium in the cosmic gravitational background (CGB). The calculation closely follows the derivation of the energy density of stochastic electromagnetic fields in Ref. [
49] and gives the same dependence of energy density on dipole gravitational fields as was derived in App. K.
Consider a 1-dimensional oscillator with mass , amplitude , and mass dipole moment,
.(P.1)
The power dissipated through (nonrelativistic) dipole radiation, from (K.10), is
,(P.2)
where .
The power dissipated through dipole radiation, by integration by parts, from (P.2), is
.(P.3)
The dissipative force, from (P.1) and (P.3), is
.(P.4)
The equation of motion of a 1-dimensional oscillator of resonant angular frequency , driven by a dipole gravitational wave of force and polarized in the direction, from (P.1) and (P.4), is
.(P.5)
The time-averaged dipole power radiated from the oscillator at resonance in steady state, from (P.1) and (P.5), is
,(P.6)
in agreement with (N.8).
The oscillator radiation resistance,
, the real part of radiation impedance, is the in-phase component of
divided by
, Ref. [
49], from (P.1) and (P.4),
,(P.7)
where is the damping constant from (N.13).
Radiation resistance implies there exists a randomly fluctuating gravitational force
in the
direction on the mass
, and therefore a randomly fluctuating gravitational field
, such that, from Ref. [
49],
,(P.8)
where and the integral over in (P.8) is .
The mean-square fluctuating gravitational field of the CGB is
,(P.9)
where is the gravimagnetic field from (J.8).
The mean energy density of the CGB, from (J.8), (P.8) neglecting the zero-point contribution, and (P.9), is
,(P.10)
in agreement with the Stefan-Boltzmann law (O.8).
The rms fluctuating gravitational field of the CGB, from (P.10), is
.(P.11)
The mean energy density of the cosmic microwave background (CMB) at equilibrium temperature , corresponding to (P.10), in terms of the root-mean-square (rms) electric and magnetic fields of the CMB, is
.(P.12)
Appendix Q. Drag on Particles in the CGB
This appendix calculates the dipole gravitational radiation of particles moving through the cosmic gravitational background (CGB) and acted on by no forces other than the dipole gravitational forces produced by the stochastic gravitational and gravimagnetic fields of the CGB.
The total instantaneous dipole gravitational power radiated into the radiation zone by an isolated nonrelativistic particle of mass having an acceleration , from Eq. (23), is
. (Q.1)
As shown in
Table 1, (Q.1) corresponds to the familiar Larmor result for the total electro mag netic dipole power,
, radiated by a nonrelativistic accelerated charge
.
The Lorentz invariant generalization of (Q.1) is
, (Q.2)
where the momentum 4-vector of the particle is ; the velocity 3-vector is ; the Lorentz factor is ; is the proper time; and is the proper time element.
The electromagnetic power radiated by an accelerating particle of charge
, corresponding to (Q.2), was first obtained by Liénard in 1898, as recounted in Ref. [
22], as
. (Q.3)
The proof of the uniqueness of this Lorentz invariant generalization for Larmor radiation power, given in Ref. [
22], also applies to dipole gravitational radiation power
in (Q.2).
By symmetry in a static, homogeneous universe, the net drag force of the CGB on a particle is expected to be anti-parallel to the velocity of the particle, so from (Q.2),
,(Q.4)
where is the Lorentz factor. For slow particles, (Q.4) agrees with (Q.1).
The manifestly covariant electromagnetic equation of motion is, from Ref. [
22],
,(Q.5)
where is the 4-velocity of the charge , and is the electromagnetic field-strength tensor.
In terms of electric and magnetic fields, and , through which the charge is moving, the radiated electromagnetic power, from (Q.3) and (Q.5), is
,(Q.6)
where and are the components of the electric field perpendicular to, and parallel to, the velocity of the charge, and is the component of the magnetic field perpendicular to the velocity of the charge.
In terms of gravitational and gravimagnetic fields, and , through which a mass is moving, the total instantaneous dipole gravitational power, from (Q.2) and App. K, and corresponding to (Q.6), is
,(Q.7)
where and are the components of the gravitational field perpendicular to, and parallel to, the velocity of the mass, and is the component of the gravimagnetic field perpendicular to the velocity of the mass.
The total instantaneous dipole gravitational power radiated by a slow particle, for which and , moving through combined gravitational and gravimagnetic fields, for which is comparable to , from (Q.6), is
for .(Q.8)
For a slow particle, the gravimagnetic field components, and , produce negligible and zero radiated power, respectively, as long as is not much greater than .
The mean dipole gravitational power radiated by a slow particle moving through the stochastic gravitational field of the CGB, from (Q.8), is
.(Q.9)
Numerical simulations confirm that the mean-square stochastic gravitational field of the CGB, , has the same effect on the energy of slow particles over long periods of time as the constant mean-square gravitational field of the CGB, .
Therefore, from (Q.1) and (Q.9), a slow particle moving through the CGB radiates the same dipole gravitational power, independent of velocity, as a particle subject to a constant dissipative deceleration
.(Q.10)
In the CGB at an equilibrium temperature , the blackbody gravitational and gravimagnetic fields of the CGB have a mean energy density , given by the Stefan-Boltzmann law, Eq. (O.8). Therefore, the deceleration, which is the rms fluctuating gravitational field of the CGB, from (P.11), is
.(Q.11)
The next appendix, App. R, calculates the exact metric of a static, homogeneous universe, from which a nondissipative, curvature-related deceleration constant is calculated. In App. S, this nondissipative, curvature-related constant is shown to be an invariant scalar equal to , where is the Hubble constant. In App. T, the dissipative deceleration constant in (Q.11) will be shown to be equal to the curvature-related deceleration constant in a static, homogeneous universe.
Appendix R. Exact Metric of a Static, Homogeneous Universe
This appendix summarizes the derivation of an exact solution in isotropic Cartesian coordinates of Einstein’s equation for a static (time-independent and time-reversible), homogeneous spacetime. In isotropic Cartesian coordinates, , the most general static, homogeneous spacetime interval is
,(R.1)
where is the proper time element; and and are functions of , the displacement 3-vector from the origin .
The general solution of Einstein’s equation for a spacetime interval of the form (R.1) is derived in Ref. [
33]. This appendix considers only the simple special case,
, of coordinates for which the 3-volume is flat. That is, the only nonvanishing components of the metric tensor are the diagonal components,
.(R.2)
The Christoffel symbols are defined in Ref. [
3], for example, as
,(R.3)
where a comma denotes partial differentiation, as for example, . With the metric in (R.2), all but nine of the 64 Christoffel symbols vanish identically,
(R.4)
where a subscript coordinate, ,, or , indicates partial differentiation with respect to that coordinate, as for example, .
The Riemann curvature tensor,
,(R.5)
has the three independent components,
(R.6)
The other components needed for the contraction of the Riemann tensor to the Ricci tensor, , are found from the identities and . Then the only components of the Ricci tensor that do not vanish identically are the diagonal components,
.(R.7)
The curvature scalar , which is the contraction of the Ricci tensor, from (R.7), is
.(R.8)
Ein stein’s equation is
,(R.9)
where is the cosmological constant; , the four-dimensional Kronecker delta, is 1 if and 0 otherwise; is the energy-momen tum tensor; and .
Symmetry requires and . Einstein’s equation requires , and both sides of this equation transform as a scalar only if , so that . Then , and the curvature scalar, from (R.8) and (R.9), is
.(R.10)
A positive energy density, , requires negative curvature, , and negative cosmological constant, .
Any ray from the origin may be defined as the positive axis in Cartesian coordinates, so Einstein’s equation, (R.9), along any ray from the origin becomes
.(R.11)
The exact general solution of (R.11) along any ray from the origin is
,(R.12)
where is an invariant distance from any origin to its event horizon; , or alternatively , is a dimensionless curvature constant; and and are dimensionless constants determined by the boundary conditions, at and at .
Then the exact diagonal metric of a static, homogeneous universe with a flat 3-volume may be expressed in Cartesian coordinates along any ray from the origin, from (R.2) and (R.12), as
.(R.13)
The component of the metric is plotted in Fig. 5 in Sec. 3.9.
Appendix S. Hubble Redshift and Apparent Cosmic Acceleration in a Static Universe
From the metric (R.13), this appendix calculates the effects of a static, homogeneous distribution of energy density throughout a static universe on propagation of light. The spacetime curvature of a static universe causes a time dilation of clocks increasing with their distance that accounts for the Hubble redshift and for an apparent cosmic acceleration.
Section 3.12 and App. U show that the appearance of cosmic acceleration in a static universe fits SN-Ia light curve data well for a narrow range of possible energy densities in the static universe.
In isotropic Cartesian coordinates, , the spacetime interval derived in (R.13) for a static, homogeneous universe with a flat 3-volume is
,(S.1)
where is the proper time element. The exact diagonal metric of a static, homogeneous universe with a flat 3-volume, expressed in Cartesian coordinates along any ray from the origin, from (R.13), is
,(S.2)
where is the Cartesian coordinate distance along any ray from the origin; is a convenient function for these calculations; is the distance to the event horizon, at which ; is a dimensionless curvature constant; the curvature scalar is the trace of the Ricci tensor ; and is the homogeneous total energy density of the universe.
The time dilation of clocks at rest in a static universe, , as seen by an observer at rest at the origin, depends upon their distance from the origin, from (S.1) and (S.2), as
.(S.3)
where .
For an observer at rest at the origin in a static, homogeneous universe, the exact redshift parameter, from (S.3), is
.(S.4)
For all over short ranges, , the redshift parameter is linear with range to lowest order in . To second order in , (S.4) becomes
.(S.5)
Over short ranges, the Hubble constant is related to the redshift parameter by , so that for , the Hubble constant is related to the curvature (and energy density) in a static universe, from (S.5), by
,(S.6)
and the redshift parameter in a static universe in terms of the Hubble constant, from (S.5) and (S.6), is expanded to second order in as
.(S.7)
Consider a pulse of light transmitted towards the origin of coordinates from a source at rest at a distance from the origin of coordinates in the rest frame of a static, homogeneous universe. The frequency of light at its source is , and the pulse duration at its source is . When this light pulse reaches an observer at rest at the origin, the frequency of the light will have been redshifted to
,(S.8)
and the pulse duration will have been lengthened to
.(S.9)
That is, time dilation in a static, homogeneous universe will have caused the energy of the light pulse at the coordinate origin to be reduced from the energy at the light source by a factor and the power of the light pulse at the origin to be reduced by a factor from the power of the pulse at the source.
Over short ranges, , the frequency redshift of light in a static universe, as a consequence of the curvature and energy density of the static universe, from (S.6) and (S.8), is given by
,(S.10)
which is just the Hubble redshift, even though the source of light is not moving with respect to the observer at the origin.
From a light source that is moving radially outward from the origin with speed
in a flat spacetime, the exact Doppler-redshifted frequency of a light pulse arriving at the origin, from Ref. [
22], is
,(S.11)
where is the frequency of the light pulse emitted by the source.
If an observer at rest at the coordinate origin of the rest frame of a static, homogeneous universe misinterprets the light that is redshifted by time dilation from a stationary source as light that is Doppler redshifted by a moving source, then, from (S.8) and (S.11), the stationary source will appear to be moving away from the observer at the origin with an apparent speed given exactly by
.(S.12)
Over short ranges, , the apparent outward speed of the stationary source, from (S.6) and (S.12), is given by
.(S.13)
That is, a stationary source of light, redshifted by time dilation in a static universe, will appear to have an outward speed , given by the Hubble redshift.
To second order in , the apparent speed of a stationary source in a static universe, from (S.6), (S.7) and (S.13), is
.(S.14)
The first term on the right-hand side of (S.14) is an apparent Hubble expansion velocity proportional to distance in a static universe. The second term describes an apparent cosmic acceleration. Appendix U shows that the apparent cosmic acceleration in (S.14) fits the SN-Ia distance modulus data well over a range of from to . But this infinite range of values of corresponds to a narrow range of total density of a static universe. The range of the ratio of the total energy density of a static universe to the critical energy density of a ΛCDM universe, corresponding to , will be shown in App. U to be .
Appendix T. Particle Motion in a Static Universe With CGB Drag
This appendix calculates the combined effects on particle motion, as observed in the rest frame
of a static, homogeneous universe, of time dilation derived in App. S with the dissipative drag force of the cosmic gravitational background (CGB).
Appendix Q showed that the CGB causes a deceleration of all particles with respect to the rest frame
. This dissipative drag force of the CGB is identified in this appendix with the time-dilation drag force of the metric. This identification is possible because the kinetic energy converted to potential energy by the metric, unlike the situation in a time-reversible conservative potential, is nonrecoverable. Then the equation of motion of particles in a static, homogeneous universe relates the Hubble constant
to the root-mean-square gravitational field
of the CGB.
As in App. S, in isotropic Cartesian coordinates, , the spacetime interval derived in (R.13) for a static, homogeneous universe with a flat 3-volume is
,(T.1)
where is the proper time element. The exact diagonal metric of a static, homogeneous universe with a flat 3-volume, expressed in Cartesian coordinates along any ray from the origin, from (R.13), is
,(T.2)
where is the Cartesian coordinate distance along any ray from the origin; is a convenient function for these calculations; is the distance to the event horizon, at which ; is a dimensionless curvature constant; the curvature scalar is the trace of the Ricci tensor ; and is the homogeneous total energy density of the universe.
Let be the 4-velocity of a particle in the rest frame of a static, homogeneous universe, where an overdot indicates differentiation with respect to the proper time of the particle as, for example, ; is the instantaneous specific 3-momentum of the particle in ; and is a coordinate that keeps track of the total distance traveled by the particle in , so is always nonnegative.
The homogeneous equation of motion of a particle in a static universe is sufficient to calculate the drag on a particle moving through a static, homogeneous universe, just as the Hubble redshift of light was calculated from the metric in App. S. The time-dilation drag effect on particle motion is expressed as a dissipative drag 4-force in a flat spacetime. The drag force applied by the CGB is the physical means by which time-dilation drag is effectuated. As a result of deceleration by the CGB, the particle radiates. The additional energy loss and deceleration of the particle by dipole radiation is calculated at the end of this appendix.
For an observer at rest in , the homogeneous equation of motion of a particle of mass acted on by the time-dilation drag of the metric through the CGB is
,(T.3)
where the are the Christoffel symbols defined at (R.3) and (R.4).
In a static, homogeneous universe, with the metric component given by (T.2), and the Christoffel symbols given by (R.4), the scalar product of the 4-velocity with the homogeneous equation of motion (T.3) is
.(T.4)
The first integral of (T.4) is
,(T.5)
which agrees with the energy equation of the invariant spacetime interval (T.1) with a flat 3-volume.
The time component of the homogeneous equation of motion (T.3) is
.(T.6)
The space components of the homogeneous equation of motion (T.3), from (T.5), are
,(T.7)
where is a unit vector in the direction of the instantaneous particle velocity in .
In terms of a dimensionless specific energy , the energy equation (T.5) becomes
,(T.8)
and the space components of the homogeneous equation of motion (T.7) become
.(T.9)
Differentiating with respect to proper time, from (T.6), gives
, (T.10)
from which the specific energy appears to be a conserved quantity.
Consider a particle radially inbound to an observer at rest at the coordinate origin in a static, homogeneous universe. The particle starts an initial distance from the origin with an initial specific 3-momentum , and has just enough energy to reach the origin before coming to rest there, where and .
For a slow particle () starting close to the origin, (T.8) becomes
.(T.11)
Since is conserved for a particle that comes to rest at the origin, the range is related to the initial specific 3-momentum , from (T.11), by
,(T.12)
showing that the slow particle undergoes a constant deceleration as a result of the time-dilation drag of the metric.
But from (Q.9) and (Q.10), a slow particle moving through the CGB radiates the same dipole gravitational power, independent of velocity, as a particle subject to a constant dissipative deceleration, , where is the constant root-mean-square gravitational field of the CGB. Since the CGB is taken to be the physical mechanism by which the energy of a particle is dissipated as it moves through a static, homogeneous universe, from (Q.10) and (T.12), in a static, homogeneous universe is identified as
.(T.13)
The range of a slow particle before it is brought to rest in a static, homogeneous universe, from (T.12), is . Because the metric has a flat 3-volume, every observer at rest in a static, homogeneous universe will agree on the range of the particle.
The conserved dimensionless specific energy of an ultrarelativistic particle () inbound to an observer at the origin from a short range (), from (T.8), is
.(T.14)
Over short ranges, (T.14) shows that the loss of momentum and energy of an ultrarelativistic particle from time-dilation drag, as a consequence of the curvature and energy density of the static universe, is the same as the loss of momentum and energy (and frequency) of light, given by (S.10). That is, ultrarelativistic particles moving through a static universe experience the same energy loss as light, an energy loss described by the Hubble redshift.
For particles of any initial momentum in a static, homogeneous universe, the range of a particle which has an initial specific 3-momentum , from the energy equation (T.8), is shown in Fig. 6 in Sec. 3.11.
Although the specific energy of a particle moving through the rest frame of a static universe is ostensibly a conserved quantity, the potential energy stored in the gravitational field is nonrecoverable. Reversing the velocity of the particle through does not restore kinetic energy to the particle. Instead, kinetic energy is irrevocably lost no matter which direction the particle moves through a static universe. This behavior is characteristic of a dissipative drag force acting on particles, not of a conservative gravitational potential. Since the time-dilation drag force on a particle acts like a dissipative drag force, rather than the force of a conservative potential, it should be possible to express the time-dilation drag force in the curved spacetime of a static universe as a dissipative drag force in a flat (Minkowski) spacetime, at least over distances short compared to , the length scale of the universe.
So now let be the 4-velocity of a particle in the rest frame of a flat spacetime. For an observer at rest in , the equation of motion of a particle of mass acted on by a dissipative drag 4-force decelerating the particle is
,(T.15)
where is the dissipative drag 4-vector.
In a Minkowski metric, , the scalar product of the 4-velocity with the inhomogeneous equation of motion (T.15) is
.(T.16)
The first integral of (T.16) is
.(T.17)
The energy equation in a Minkowski metric shows from (T.17) that the drag 4-vector must be orthogonal to the particle 4-velocity, that is, .
The dimensionless specific energy of the particle is defined as . Then the time component of the inhomogeneous equation of motion (T.15) is
,(T.18)
and the space components of (T.15) are
.(T.19)
By symmetry in a flat spacetime, any particle that is acted upon only by a drag force will move along a straight trajectory. Since is anti-parallel to by symmetry, and since , then . And since , then the time and space components of the dissipation drag 4-vector are related by
.(T.20)
The time component of the drag 4-vector is a measure of power loss by the particle. For a particle at rest in , and .
If a drag scalar is defined as , then the drag 4-vector, from (T.20), is
,(T.21)
where is a unit vector in the direction of the instantaneous particle velocity in . This drag 4-vector satisfies , , and .
From (T.18) and (T.21),
, (T.22)
which has the exact solution
,(T.23)
where the initial condition was used.
For a slow particle () over a short distance (), (T.23) becomes
,(T.24)
and from (T.24),
,(T.25)
showing that the slow particle undergoes a constant deceleration as a result of the drag force.
For an ultrarelativistic particle () over a short distance (), (T.23) becomes
,(T.26)
so that an ultrarelativistic particle has a deceleration, from (T.26),
.(T.27)
But from (T.9), the deceleration of a particle of any speed over short distances is
.(T.28)
Comparing (T.27) and (T.28) gives the value of the deceleration scalar as
,(T.29)
and the dissipative drag 4-vector over short distances () associated with the 4-velocity of a particle in a static universe, from (T.21) and (T.29), is
.(T.30)
The dissipative equation of motion, , with given by (T.30), emulates the conservative energy equation (T.8), but only over distances much shorter than the cosmological length scale , and only for particles inbound to an observer at the origin. For outbound particles, (T.30) continues to make sense, because it is independent of coordinates and a metric. But for outbound particles, the energy equation (T.8) is unphysical, because there is no conservative potential in a static universe. Kinetic energy can only be lost to the gravitational field; it cannot be recovered.
The instantaneous dipole gravitational power radiated by a particle of mass decelerated by time-dilation drag in a static universe, from (Q.2) and (T.30), is
. (T.31)
and from (T.13), the instantaneous dipole gravitational power radiated by a particle of mass , decelerated by the CGB in a flat universe, is
. (T.32)
Appendix U. Appearance of Cosmic Acceleration in a Static Universe
This appendix calculates the effects of time dilation in a static universe on supernova Type Ia (SN-Ia) light curves. The model of the static universe has only one adjustable parameter, total energy density, and the fit to the SN-Ia light-curve data is good in a narrow range of this parameter.
The energy density of a static universe is related to the curvature scalar defined in (R.8) and to the cosmological constant , from (R.10), by
,(U.1)
where .
Since and , the total energy density of a static universe, including the CGB, from (S.6) and (U.1), is
,(U.2)
where is the Hubble constant, and is the time-dilation deceleration constant from (T.12).
The critical energy density
of a lambda-cold-dark-matter (ΛCDM) universe is the energy density below which a ΛCDM universe expands forever, and above which the expansion comes to a stop and reverses. From Ref. [
3] and (S.6), this critical energy density is
.(U.3)
The ratio of the total energy density of a static universe to the critical energy density of a ΛCDM universe, from (U.2) and (U.3), is
,(U.4)
showing that a static universe does not support a total energy density greater than .
But since the energy density of a static, homogeneous universe can also be expressed as
,(U.5)
where is the total mass energy of the universe within the radius , including the CGB, the ratio of energy densities in (U.4) can also be expressed as
.(U.6)
Note that is the condition for an event horizon at radius in the isotropic Cartesian coordinates of this static solution, just as is the condition for an event horizon in Schwarzschild coordinates.
From (U.4) and (U.6), , so that the ratio of the total energy density of a static universe to the critical energy density of a ΛCDM universe, from (U.4), is
.(U.7)
Figure 8 in Sec. 3.12 is a plot of the ratio
vs.
.
The energy density of the CGB, from (P.10), is
.(U.8)
The ratio of the energy density of the CGB to the critical energy density of a ΛCDM universe, from (U.3), (U.8), and (T.13), is
. (U.9)
The ratio of the energy density of the CGB to the total energy density of a static universe including the CGB, from (U.2) and (U.8), is
.(U.10)
Since the energy density of the CGB cannot exceed the total energy density of a static universe including the CGB, the lower bound on , from (U.10), is
, (U.11)
and the lower bound on the Hubble constant, from (S.6) and (U.11), is
.(U.12)
The ratio of the total energy density of a static universe to the critical energy density of a ΛCDM universe, from (U.7) and (U.9), is in the range
,(U.13)
or .
The upper bound on the value of for a static universe, from (U.12), corresponds to , and corresponds to the upper bounds, from (U.1),
.(U.14)
As shown in this appendix below, the cosmological model of a static universe fits the SN-Ia light-curve data quite well with only one adjustable parameter, total energy density (or curvature constant ), and over a broad range of .
From time dilation in a static universe, the frequency of a radially inbound photon observed at the origin is related to the frequency of that photon a distance away, from (S.8), by
.(U.15)
The pulse duration of a bunch of photons is lengthened by time dilation by the same factor as the wavelength of the photons. An incoming bunch of photons with a total energy and total power appears to lose power, from (U.15), as
,(U.16)
where is the absolute total power of the incoming photon bunch measured by an observer at the origin.
Let be the absolute luminosity, the power radiated by a supernova. Let be the apparent luminosity, the power received per unit area at the detector. The ratio, from (U.16), is
,(U.17)
The exact redshift parameter in a static, homogeneous universe, from (S.4), is
.(U.18)
The luminosity ratio in (U.17), from (U.18), becomes
.(U.19)
The apparent magnitude of an SN-Ia is . The absolute magnitude of an SN-Ia is related to its absolute luminosity by . Then the distance modulus, , defined as the difference between the apparent and absolute magnitudes, for an SN-Ia at a distance in a static universe is
,(U.20)
where is an instrument-calibration constant. This distance modulus function in (U.20) of the redshift parameter is shown in Fig. 9 in Sec. 3.12 for several values of the curvature constant in a static universe.
The constant depends only on the calibration of the detectors and not on the features of the model. The best-fit values of the instrument-calibration constant that minimize the sums of squares of deviations of the data points from the distance modulus curves in Fig. 9 are given in Table U.1.
Table U.1.
Best-fit instrument-calibration constants in column 2 that give the least root-mean-square (standard) deviations in column 4 of the distance modulus functions of (U.20) from the data points in Fig. 9 for the curvature constants in column 1. Column 3 shows that is an excellent approximation to the best-fit for all .
Table U.1.
Best-fit instrument-calibration constants in column 2 that give the least root-mean-square (standard) deviations in column 4 of the distance modulus functions of (U.20) from the data points in Fig. 9 for the curvature constants in column 1. Column 3 shows that is an excellent approximation to the best-fit for all .
|
Best fit |
|
Standard deviation |
| 0.1 |
43.78 |
38.47 |
0.466 |
| 1 |
44.22 |
43.47 |
0.394 |
| 2 |
45.08 |
44.98 |
0.349 |
| 3 |
45.86 |
45.86 |
0.343 |
| 4 |
46.48 |
46.48 |
0.342 |
| 5 |
46.96 |
46.96 |
0.342 |
| 10 |
48.46 |
48.47 |
0.342 |
For , the distance modulus curves from (U.20) in Fig. 9 are virtually indistinguishable. The reason is that for , , and over the range of redshift parameter values in Fig. 9, the distance modulus curves from (U.20) in Fig. 9 are approximately given by
.(U.21)
That is, for , the dependence of the distance modulus on is separate from the dependence on , so that an excellent approximation to the best-fit instrument-calibration constant over the range of in Fig. 9 is effectively
,(U.22)
so that the distance modulus curves for are identical, after the constant is adjusted in accordance with (U.22) to the best fit.
The fit of the distance modulus in (U.20) to the data is robust over an unlimited range of this one parameter, from to . Although the distance modulus fits the data well over an infinite range of values of , it fits the data only over a narrow range of total density of a static universe. The range of the ratio of the total energy density of a static universe to the critical energy density of a ΛCDM universe, corresponding to , from (U.4), is
.(U.23)
Appendix V. Hubble Constant, Drag Constant and CGB Temperature
This appendix summarizes some of the recent results of measurements of the Hubble constant, , and relates those measurements to the scalar time-dilation drag constant , and to the temperature of the cosmic gravitational background (CGB).
In Table 3, Sec. 3.13, the dependence of the scalar time-dilation drag constant on the Hubble constant is
.(V.1)
The mean energy density of the CGB, from the Stefan-Boltzmann law (P.10), is
,(V.2)
where is the root-mean-square gravitational field of the CGB in a static universe.
In App. T and specifically at (T.13), it was determined that is related to the Hubble constant by
.(V.3)
Then from (V.1), (V.2), and (V.3), the temperature of the CGB is related to the Hubble constant by
.(V.4)
The temperature of the CGB, according to (V.4), is given for each of the measured values of in the last column of Table 3.
Appendix W. Dipole Anisotropy of the CGB
This appendix calculates the expected anisotropy in the cosmic gravitational background (CGB). If the CGB is a collection of indistinguishable, massless, spin-1 bosons obeying photon statistics and is in thermal equilibrium at absolute temperature , just as the cosmic microwave background (CMB) is, and if the CGB is at rest with respect to the apparent rest frame of the CMB, then the fractional temperature and frequency shifts of the CGB might be expected to be the same as the fractional temperature and frequency shifts of the CMB.
To lowest order in
, the normalized speed of the Earth through the CGB, the observed temperature of the CGB with respect to the equilibrium temperature
, from Ref. [
66], is
,(W.1)
and the apparent temperature shift is
,(W.2)
where is the angle between the boson velocity and the velocity of the Earth through the CGB.
The WMAP satellite experiment [
67] found
for a velocity of the solar system with respect to the CMB of 370 km/s. If the velocity of the solar system with respect to the CMB is the same with respect to the CGB, then the maximum temperature increase of the CGB would be
times the equilibrium temperature of the CGB. From (W.2) and Table 3, the maximum temperature increase of the CGB from the dipole anisotropy is about
. (W.3)
Appendix X. Hubble Constant Related to Planck’s Constant by the CGB
Appendix V, and specifically (V.3) related the scalar time-dilation drag constant in (S.36) for a slow particle moving through a static, homogeneous universe to the dissipative deceleration of a slow particle moving through the root-mean-square gravitational field of the cosmic gravitational background (CGB), by
.(X.1)
One result of (X.1) is that the Hubble constant is related to Planck’s constant , from (Q.11), by
.(X.2)
And the stochastic vector field of the CGB is related to the Hubble constant in turn by (X.1).
The Hubble constant and the rms field of the CGB are related to the equilibrium temperature of the CGB, from (V.3), (V.4), and (X.1), by the relations
.(X.4)
The mean total energy density of the CGB in all frequencies is given by the Stefan-Boltzmann law, from (O.8),
.(X.5)
Table 4, Sec. 3.13, shows the dependence of the mean total energy density of the CGB on the tempera ture from (X.5), and indirectly on the measured values of the Hubble constant from (X.4).
Then with the range of temperatures in Table 4, T = 21
1 K, corresponding to the range of values of the Hubble constant,
, given by Refs. [
58,
59], the mean total energy density of the CGB, from (X.5), is
;(X.6)
the limit on the total energy density of a static universe, from (U.13), is
;(X.7)
and the critical energy density of a lambda-cold-dark-matter (ΛCDM) universe, from (U.3), is
.(X.8)
The ratio of the energy density of the CGB to the critical energy density of a ΛCDM universe, from (U.9), is
, (X.9)
and the ratio of to the total energy density of a static universe including the CGB, from (U.10), is
.(X.10)
But if is greater than 2, as suggested by App. U, then, from (X.10),
.(X.11)
And in that case, any other constituent of a static universe, like ordinary mass, has an energy density satisfying
,
or
.(X.12)
That is, ordinary mass in a static universe has an energy density
no more than about 4.0 to 5.5 percent of the critical energy density
of a ΛCDM universe. This small energy density of ordinary mass
corresponds to the energy density of ordinary mass in our universe of 4.9 percent of the critical energy density
of a ΛCDM universe, for example, as inferred by Ref. [
57], and as shown graphically in Fig. 10 in Sec. 3.12.
Appendix Y. Mean Energy of an Oscillator in the CGB
The stochastic gravitational vector fields of the cosmic gravitational background (CGB) will cause every particle to undergo stochastic motion, in accordance with the equation of motion, Eq. (24). This appendix calculates an effective diffusion coefficient from the mean energy of an oscillator of resonant frequency in the CGB at equilibrium temperature . The oscillator is driven by the stochastic dipole gravitational fields of the CGB and its motion is damped by dipole radiation produced by its own acceleration.
In App. N, the derivation of the mean energy of mass oscillators in the CGB closely followed the derivation of the mean energy of oscillators in electromagnetic fields from the generalized Nyquist relation in Ref. [
49]. To recap results of App. N, the displacement
of a one-dimensional simple harmonic oscillator of mass
, resonant angular frequency
, and damping constant
, driven by a dipole gravitational wave
with constant amplitude
and polarization in the
direction, satisfies the equation of motion (N.1), and the solution of (N.1) is given by (N.2).
When driven at the resonant frequency, , the displacement of the mass , from (N.2), is
,(Y.1)
and the velocity is
.(Y.2)
The damping constant was found at (N.13) to be
.(Y.3)
When driven by a dipole gravitational wave at the resonant frequency, the total energy of the oscillator of mass , kinetic plus potential, from (Y.2), is
.(Y.4)
The line width , defined as the full width at half-maximum (FWHM) of the energy spectrum of the oscillator for , was found from (N.14) to be
.(Y.5)
Defined in this way, the line width is equal to the damping constant of an oscillator in the CGB.
The root-mean-square (rms) displacement of the oscillator from (Y.1) is . The root-mean-square speed of the oscillator from (Y.2) is . The “diffusion coefficient,” , of the oscillator is defined as the product in the CGB of “uncertainty” of oscillator position, , and “uncertainty” of oscillator speed, , or from (Y.4),
.(Y.6)
If is the zero-point energy of the one-dimensional oscillator, , then the “diffusion coefficient” from (Y.6) is
. (Y.7)
According to Ref. [
69], any particle of mass
that is constantly undergoing a Brownian motion with diffusion coefficient
obeys the Schrödinger wave equation. One might therefore conclude from (Y.7) and Ref. [
69] that an oscillator immersed in the CGB obeys the Schrödinger wave equation.
Following is an approximate derivation of the diffusion coefficient of an oscillator immersed in the CGB that involves somewhat less circular reasoning than the derivation of (Y.7). According to Planck’s second quantum theory [
117], the mean energy at the temperature
of an oscillator at natural frequency
is
.(Y.8)
In the CGB, the mean-square gravitational field polarized in the direction, from the Nyquist relations, is
.(Y.9)
Only the CGB modes roughly within the frequency band about the resonant frequency contribute significantly to the resonant amplitude of the oscillator. Consider an in-band plane-wave dipole gravitational field of the CGB,
for ,(Y.10)
propagating in the direction, comprising field modes of both polarizations, where is the amplitude, is the angular frequency, and is the phase of the field mode.
As long as
and
, then from Ref. [
33] the field modes within the narrow resonant frequency band about
combine to produce effectively a single mode with an angular frequency about equal to
and with an amplitude
, where
is the mean amplitude of each of the
modes in the narrow band. That is, within the frequency band about
, the driving field at a particular location is
,(Y.11)
where is some phase angle.
Thus, the in-band gravitational wave amplitude from (Y.1) and (Y.11) is approximately related to the in-band mean-square gravitational field, from (Y.9), by
.(Y.12)
At high resonant frequencies (), the mean energy of the oscillator is , the zero-point energy of the oscillator. Then using and using (Y.5) for the line width and for the damping constant , the in-band mean-square gravitational field from (Y.12) becomes
.(Y.13)
Then the approximate diffusion coefficient of a 1-dimensional oscillator immersed in the CGB, from (Y.6) and (Y.13), is
.(Y.14)
The reason the approximate diffusion coefficient in (Y.14) underestimates the diffusion coefficient in (Y.7) by a factor is because only those dipole wave modes within a bandwidth about the resonant frequency were taken to contribute to the gravitational wave driving the oscillator at resonance.
The diffusion coefficient of the one-dimensional oscillator in the CGB from (Y.6) is , which is independent of the stochastic vector field that produced it. The diffusion coefficient of a one-dimensional charged-particle oscillator in the stochastic electromagnetic field of the cosmic microwave background (CMB) is the same as it is in the CGB, . The reason is that the mean energy density of the CGB, from (P.10),
,(Y.15)
is the same as the mean energy density of the CMB, from (P.12),
,(Y.16)
differing only in the absolute temperature of the stochastic vector field.
And for the same reasons, the mean energy in the CGB of a one-dimensional, charged or uncharged particle oscillator at natural frequency , from (Y.8), is
,(Y.17)
while the mean energy in the CMB of a one-dimensional, charged particle oscillator at natural frequency , is
,(Y.18)
again differing only in the absolute temperature of the stochastic vector field.
At high resonant frequencies (), the mean energy of a one-dimensional charged particle oscillator is the zero-point energy of the oscillator, , in either the CGB or the CMB or both. At high frequencies, the mean energy is completely independent of the stochastic vector field that determines it. The only differences in the mean energy of oscillators arise for weakly bound or free particles, that is, for less than or about equal to .
If , then the mean energy in the CGB of a one-dimensional oscillator, from (Y.17), is about , and the mean energy in the CMB, from (Y.18), is about , differing only in the absolute temperature of the stochastic vector field. Since the absolute temperature of the CMB is and the absolute temperature of the CGB in a static universe is about , as shown in Table 3, the mean energy in a combined CGB and CMB of a free or weakly-bound, charged or uncharged, one-dimensional particle oscillator with , from Eq. (90), is about , as shown in Fig. 11, Sec. 3.14.