Investigation of Natural Transition on a Sharp Leading Edge Flat Plate in a Hypersonic Shock Tunnel
Author:
Affiliation:
1. Indian Institute of Science
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3096
Reference10 articles.
1. Stetson,K.F."HypersonicBoundaryLayerTransition,"1992.
2. Summary of Hypersonic Transition Research Coordinated Through NATO RTO AVT-136
3. Dennis C. Berridge, R. P. L. A. C. A. D. A., Christopher A.C. Ward, and Schneider, S. P. "Boundary-Layer Instability MeasurementsinaMach-6QuietTunnel,"42ndAIAAFluidDynamicsConferenceandExhibit,25-28June2012.
4. Guillaume Grossir, D. M., and Chazot, O. "Flow characterization and boundary layer transition studies in VKI hypersonic facilities,"53rdAIAAAerospaceSciencesMeeting,Kissimmee,Florida,5-9January2015.
5. Kennedy, R. E., Stuart J. Laurence, M. S. S., and Marineau, E. C. "Hypersonic Boundary-Layer Transition Features from High-SpeedSchleirenImages,"55thAIAAAerospaceSciencesMeeting,Grapevine,Texas,9-13January2017.
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