High-Bandwidth Optical Measurements of the Second-Mode Instability in a Mach 6 Quiet Tunnel
Author:
Affiliation:
1. Texas A&M University
2. Cornell University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-378
Reference28 articles.
1. Boedeker, L. R. 1959. Analysis and Construction of a Sharp Focussing Schlieren System. M.S. Thesis.Massachusetts Institute of Technology.
2. NASA Langley Mach 6 Quiet Wind-Tunnel Performance
3. A Modified Schlieren Apparatus for Large Areas of Field
4. Chen F-J., Wilkinson S. P. & Beckwith, I. E. 1993. Görtler Instability and Hypersonic Quiet Nozzle Design. J. Spacecraft and Rockets30(2):170-175.
5. Chokani, N. D.1999. NonlinearSpectral Dynamics of Hypersonic Boundary LayerFlow. Phys.Fluids11(12):3846-3851.
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