Numerical and experimental investigation of CO2 condensate behavior in hypersonic flow
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
2. Princeton Univ., NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2379
Reference49 articles.
1. Development of planar diagnostics for imaging Mach 8 flowfields using carbon dioxide and sodium seeding
2. Physical model of the swept shock wave/boundary-layer interaction flowfield
3. Study of compressible mixing layers using filtered Rayleigh scattering based visualizations
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