Crossflow Transition on a Pitched Cone at Mach 8
Author:
Affiliation:
1. Sandia National Laboratories
2. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4299
Reference39 articles.
1. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
2. Disturbance growth in an unstable three-dimensional boundary layer and its dependence on environmental conditions
3. Traveling Crossflow Instability for the HIFiRE-5 Elliptic Cone
4. Freestream Effects on Boundary Layer Disturbances for HIFiRE-5
5. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability
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1. Effect of Freestream Noise on Hypersonic Crossflow-Induced Boundary-Layer Transition;AIAA Journal;2022-12
2. Using Discrete and Distributed Roughness to Generate Stationary Crossflow Waves in a Mach 6 Quiet Tunnel;AIAA Aviation 2019 Forum;2019-06-15
3. Hypersonic Crossflow Instability;Journal of Spacecraft and Rockets;2019-03
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