Towards Global Stability Analysis of Flexible Aircraft in Edge-of-the-Envelope Flow
Author:
Affiliation:
1. University of Liverpool
Publisher
American Institute of Aeronautics and Astronautics
Reference47 articles.
1. Global instability of wing shock-buffet onset
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1. Global Stability Analysis of Full-Aircraft Transonic Buffet at Flight Reynolds Numbers;AIAA Journal;2023-10
2. Global stability analysis of elastic aircraft in edge-of-the-envelope flow;Journal of Fluid Mechanics;2023-07-12
3. Shock Buffet and Associated Fluid–Structure Interactions of the Benchmark Supercritical Wing;AIAA Journal;2023-05
4. Resolvent analysis of a finite wing in transonic flow;Flow;2023
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