Heat Flux on a Hypersonic Cone with a Highly Swept Fin
Author:
Funder
Office of Naval Research
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.A35410
Reference48 articles.
1. Some aspects of shock-wave boundary layer interaction at hypersonic speeds
2. Survey of viscous interactions associated with high Mach number flight
3. Wavelet Analysis of Wall-Pressure Fluctuations in a Supersonic Blunt-Fin Flow
4. Laminar boundary layer separation at a fin-body junction in a hypersonic flow
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2. Crossflow Instability on a Swept Fin–Cone with Variable Nose Bluntness in Mach 6 Flow;AIAA Journal;2024-06
3. Boundary-layer instability on a highly swept fin on a cone at Mach 6;Journal of Fluid Mechanics;2024-05-16
4. Cross-flow instability on a swept-fin cone at Mach 6: characteristics and control;Journal of Fluid Mechanics;2024-02-21
5. Comparative Studies on the Hypersonic Finned Cone;AIAA SCITECH 2023 Forum;2023-01-19
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