History and Progress of Boundary-Layer Transition on a Mach-6 Flared Cone
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana 46556
2. Johns Hopkins University, Laurel, Maryland 20723
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34285
Reference57 articles.
1. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
2. Transition and Stability of High-Speed Boundary Layers
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels
5. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
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