Instability and Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0355
Reference13 articles.
1. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels
2. 2Schneider, S. P. “Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes,” AIAA-2005-4763 , June
3. Numerical Investigation of Laminar-Turbulent Transition in a Cone Boundary Layer at Mach 6
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