Receptivity to Freestream Acoustic Noise in Hypersonic Flow over a Generic Forebody
Author:
Affiliation:
1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
2. MBDA-France, 92350 Le Plessis-Robinson, France
3. MBDA-France, 18020 Bourges, France
4. MBDA UK, Ltd., Filton, England BS34 7QW, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34283
Reference53 articles.
1. On the breakdown of boundary layer streaks
2. Transition of streamwise streaks in zero-pressure-gradient boundary layers
3. BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES
4. Prehistory of Instability in a Hypersonic Boundary Layer
5. Transition and Stability of High-Speed Boundary Layers
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1. Direct Numerical Simulation of Acoustically-Driven Transition in a Hypersonic Wind Tunnel;AIAA AVIATION 2023 Forum;2023-06-08
2. Roughness-Induced Instabilities and Transition on a Generic Hypersonic Forebody at Mach 6;AIAA Journal;2021-09
3. Effects of Freestream Acoustic Disturbances on Hypersonic Boundary Layer Stability;AIAA AVIATION 2020 FORUM;2020-06-08
4. Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise;Journal of Fluid Mechanics;2020-06-04
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