Instability Measurements on a Cone-Slice-Flap in Mach-6 Quiet Flow
Author:
Affiliation:
1. Purdue University
2. University of Liverpool
3. Polytechneio Kretes
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0500
Reference40 articles.
1. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
2. Hypersonic and High-Temperature Gas Dynamics, Third Edition
3. Experimental Studies of Shock Wave???Boundary-Layer Interactions in Hypersonic Flows
4. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
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1. Relaminarization effects in hypersonic flow on a three-dimensional expansion–compression geometry;Journal of Fluid Mechanics;2024-04-22
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