Time-sequenced and spectrally filtered Rayleigh imaging of shock wave and boundary layer structure for inlet characterization-Reference-Cited by-同舟云学术

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Time-sequenced and spectrally filtered Rayleigh imaging of shock wave and boundary layer structure for inlet characterization

Published:1993-06-28 Issue: Volume: Page:
ISSN:
Container-title:29th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

FORKEY JOSEPH¹,COGNE SANDRINE¹,SMITS ALEXANDER¹,BOGDONOFF SEYMOUR¹,LEMPERT WALTER¹,MILES RICHARD¹

Affiliation:

1. Princeton Univ., NJ

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2300

Reference7 articles.

1. Rayleigh imaging and flow tagging in ground test facilities

2. S. Cogne, J. Forkey, W. Lempert, R.B. Miles, and AJ. Smits,"TheEvolutionofLarge-ScaleStructuresina Supersonic Turbulent Boundary Layer," ASME Fluids EngineeringConf.,WashingtonD.C.,June 20-%,1993.

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