Instability and Transition on a Cone with a Slice and Ramp at Mach 6
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Reference28 articles.
1. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
2. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels
3. Development of U.S. Air Force Intercontinental Ballistic Missile Weapon Systems
4. Experimental Studies of Shock Wave???Boundary-Layer Interactions in Hypersonic Flows
5. X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography
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2. Instability and transition onset downstream of a laminar separation bubble at Mach 6;Journal of Fluid Mechanics;2023-08-15
3. Instability and Transition Onset Downstream of an Axisymmetric Separation Bubble with Sharp and Blunt Nosetips;AIAA AVIATION 2023 Forum;2023-06-08
4. Relaminarization Effects on a Three-Dimensional Cone-Slice-Ramp Geometry at Mach 8;AIAA SCITECH 2023 Forum;2023-01-19
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