Nonlinear Aeroelastic Reduced-Order Modeling Approach with Geometric Gradient Computation Capability

2021 ◽  
Author(s):  
Jeffrey Thomas ◽  
Earl H. Dowell
2020 ◽  
Vol 141 ◽  
pp. 107321 ◽  
Author(s):  
Fahad Alsayyari ◽  
Marco Tiberga ◽  
Zoltán Perkó ◽  
Danny Lathouwers ◽  
Jan Leen Kloosterman

2016 ◽  
Vol 71 (11) ◽  
pp. 2155-2169 ◽  
Author(s):  
Jeff Borggaard ◽  
Zhu Wang ◽  
Lizette Zietsman

2013 ◽  
Vol 2013 ◽  
pp. 1-12 ◽  
Author(s):  
Ibrahim Yilmaz ◽  
Ece Ayli ◽  
Selin Aradag

Simulations of supersonic turbulent flow over an open rectangular cavity are performed to observe the effects of length to depth ratio (L/D) of the cavity on the flow structure. Two-dimensional compressible time-dependent Reynolds-averaged Navier-Stokes equations with k-ωturbulence model are solved. A reduced order modeling approach, Proper Orthogonal Decomposition (POD) method, is used to further analyze the flow. Results are obtained for cavities with severalL/Dratios at a Mach number of 1.5. Mostly, sound pressure levels (SPL) are used for comparison. After a reduced order modeling approach, the number of modes necessary to represent the systems is observed for each case. The necessary minimum number of modes to define the system increases as the flow becomes more complex with the increase in theL/Dratio. This study provides a basis for the control of flow over supersonic open cavities by providing a reduced order model for flow control, and it also gives an insight to cavity flow physics by comparing several simulation results with different length to depth ratios.


AIAA Journal ◽  
2018 ◽  
Vol 56 (12) ◽  
pp. 5041-5044 ◽  
Author(s):  
Pinar Acar ◽  
Veera Sundararaghavan

AIAA Journal ◽  
2012 ◽  
Vol 50 (2) ◽  
pp. 366-374 ◽  
Author(s):  
Andrew Madden ◽  
Bogdan I. Epureanu ◽  
Sergio Filippi

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