Preprint Review Version 2 Preserved in Portico This version is not peer-reviewed

An Explanation and Understanding of Aerodynamic Lift by Triple Deck Theory

Version 1 : Received: 19 May 2021 / Approved: 21 May 2021 / Online: 21 May 2021 (07:42:58 CEST)
Version 2 : Received: 2 November 2021 / Approved: 9 November 2021 / Online: 9 November 2021 (14:52:31 CET)

How to cite: Schaffarczyk, A. An Explanation and Understanding of Aerodynamic Lift by Triple Deck Theory. Preprints 2021, 2021050496. https://doi.org/10.20944/preprints202105.0496.v2 Schaffarczyk, A. An Explanation and Understanding of Aerodynamic Lift by Triple Deck Theory. Preprints 2021, 2021050496. https://doi.org/10.20944/preprints202105.0496.v2

Abstract

An explanation of aerodynamic lift still is under controversial discussion as can be seen, for example, in a recent published article in Scientific American [1]. In contrast to an approach via integral conservation laws we here review an approach via the classical Kutta-Condition and its relation to boundary layer theory. Thereby we summarize known results for viscous correction to the lift coefficient for thin aerodynamic profiles and try to remember the work on triple-deck or higher order Boundary Layer theory, its connection to interactive boundary layer theory, viscous/inviscid coupling as implemented to well-known engineering code Xfoil. Finally we compare its findings to simple 2D numerical solution of full Navier Stokes equations (CFD)models. As a conclusion, a clearer definition of terms like understanding and explanation applied to the phenomenon of aerodynamic lift will be given.

Keywords

Aerodynamic Lift; Boundary Layer Theory; Triple Deck Theory

Subject

Engineering, Mechanical Engineering

Comments (1)

Comment 1
Received: 9 November 2021
Commenter: Alois Peter Schaffarczyk
Commenter's Conflict of Interests: Author
Comment: As stated in the footnote of the title, the manuscript has been updated according the the remarks of the reviewers. Keywords have been added
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