Version 1
: Received: 2 May 2019 / Approved: 6 May 2019 / Online: 6 May 2019 (10:29:25 CEST)
How to cite:
Ghalandari, M.; Ziamolki, A.; Mosavi, A.; Shamshirband, S.; Chau, K. Aeromechanical Optimization of First Row Compressor Test Stand Blades. Preprints2019, 2019050049. https://doi.org/10.20944/preprints201905.0049.v1
Ghalandari, M.; Ziamolki, A.; Mosavi, A.; Shamshirband, S.; Chau, K. Aeromechanical Optimization of First Row Compressor Test Stand Blades. Preprints 2019, 2019050049. https://doi.org/10.20944/preprints201905.0049.v1
Ghalandari, M.; Ziamolki, A.; Mosavi, A.; Shamshirband, S.; Chau, K. Aeromechanical Optimization of First Row Compressor Test Stand Blades. Preprints2019, 2019050049. https://doi.org/10.20944/preprints201905.0049.v1
APA Style
Ghalandari, M., Ziamolki, A., Mosavi, A., Shamshirband, S., & Chau, K. (2019). Aeromechanical Optimization of First Row Compressor Test Stand Blades. Preprints. https://doi.org/10.20944/preprints201905.0049.v1
Chicago/Turabian Style
Ghalandari, M., Shahab Shamshirband and Kwok-Wing Chau. 2019 "Aeromechanical Optimization of First Row Compressor Test Stand Blades" Preprints. https://doi.org/10.20944/preprints201905.0049.v1
Abstract
In this study, an optimization of the first blade in new test rig presented. Blade tuning is conducted using 3D geometrical parameters. Sweep and dihedral play an essential role in this study. Compressor characteristics and blades vibrational behavior are the main objective of the evaluation. Here, the attachments are designed to isolate blade dynamics from Disk. So, the Vibrational behaviors of the one's blade are tuned based on the self-excited and forced vibration phenomenon. Using a semi analytical MATLAB code instability conditions are satisfied. The code takes advantages of whitehead and force response theory to predict classically and stall flutter speeds. Beside, Forced vibrations instability is controlled using a theory presented by Campbell. Aerodynamics of new blade geometry determined using multistage simulations Computational fluid dynamics (CFD) software. Numerical results show increasing performance near the surge line and working interval along with increasing mass flow.
Copyright:
This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
