Laminar to turbulent transition on the HIFiRE-1 cone at Mach 7 and high angle of attack
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. National Research Council
3. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0428
Reference11 articles.
1. Hypersonic International Flight Research and Experimentation (HIFiRE) Fundamental Science and Technology Development Strategy
2. Hypersonic International Flight Research and Experimentation Technology Development and Flight Certification Strategy
3. Aerothermodynamic Testing and Boundary-Layer Trip Sizing of the HIFiRE Flight 1 Vehicle
4. Effect of Freestream Noise on Roughness-Induced Transition for a Slender Cone
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