Measurements of Second-Mode Dominated Transition on a Straight Cone in the Boeing/AFOSR Mach-6 Quiet Tunnel
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Reference10 articles.
1. On the application of linear stability theory to the problem of supersonic boundary-layer transition
2. 2Mack, L. M. “Boundary-Layer Linear Stability Theory,” Special Course on Stability and Transition of Laminar Flow, AGARD Report 709 , March 1984, pp.1-81.
3. Transition and Stability of High-Speed Boundary Layers
4. Development of Hypersonic Quiet Tunnels
5. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Numerical Investigations of Nonlinearly Generated Disturbance Waves in High-Speed Boundary Layers;AIAA Journal;2023-11
2. Numerical Investigation of Nonlinear Boundary-Layer Transition for Cones at Mach 6;AIAA Journal;2021-06
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