Shock-tunnel flow visualization with a high-speed schlieren and laser holographic interferometry system

20th AIAA Advanced Measurement and Ground Testing Technology Conference

Volumn , Issue , 1998, Pages

  Tsai, C Y ^a   Bakos, R J ^a  

^a GASL Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT SIMULATORS; HOLOGRAPHIC INTERFEROMETRY; HOLOGRAPHY; INTERFEROMETRY; NASA; OPTICAL SYSTEMS; RAMJET ENGINES; TESTING;

FLIGHT SIMULATION; LASER HOLOGRAPHIC INTERFEROMETRY; OPERATING MODES; REFLECTED SHOCKS; SCRAMJET ENGINES; TEST SECTIONS; UNSTEADY BEHAVIORS; VISUALIZATION SYSTEM;

FLOW VISUALIZATION;

EID: 85086950758     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2700     Document Type: Conference Paper

References (12)

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7. Burner, A.W. and Goad, W.K., "Combined Single- Pulse Holography and Time-Resolved Laser Schlieren for Flow Visualization," NASA Technical Memorandum 83109, 1981.
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11. Orth, R.C. and Kislykh, V.V., "American/Russian Hypersonic Combustion Research in the TSNIIMASH PGU-11 Facility," AIAA-95-0686, 33rd Aerospace Sciences Meeting and Exhibit, January 1995.
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