Quantitative visualization of supersonic flow using Rayleigh scattering
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
2. Princeton Univ., NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-436
Reference32 articles.
1. S. M. Bogdonoff. The design, construction, and operation of the Princeton 4 by 8 inch variable-density wind tunnel. Technical Report 34, Project Squid, 1951.
2. Two- and three-dimensional effects in the supersonic mixing layer
3. The characteristics and evolution of large‐scale structures in compressible mixing layers
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