Supersonic Flutter Analysis of Vehicles at Incidence Based on Local Piston Theory
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031465
Reference9 articles.
1. Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow
2. Dynamics and Aeroelastic Analysis of Missiles
3. CFD-based aeroelastic analysis of the X-43 hypersonic flight vehicle
4. Computational Fluid Dynamics-Based Aeroservoelastic Analysis with Hyper-X Applications
5. Some Computational Aeroelastic Results for a Low Sweep Delta Wing at High Angle of Attack (Invited)
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1. Experimental and Numerical Flutter Analysis Using Local Piston Theory with Viscous Correction;Aerospace;2023-10-06
2. Rapid Steady-State Hypersonic Aerothermodynamic Loads Prediction Using Reduced Fidelity Models;Journal of Aircraft;2021-05
3. Flutter and Limit Cycle Oscillations of Cantilevered Plate in Supersonic Flow;Journal of Aircraft;2021-03
4. Enriched Piston Theory for Expedient Aeroelastic Loads Prediction in the Presence of Shock Impingements;AIAA Journal;2019-03
5. Role of Higher-Order Terms in Local Piston Theory;Journal of Aircraft;2019-01
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