Development of planar diagnostics for imaging Mach 8 flowfields using carbon dioxide and sodium seeding-Reference-Cited by-同舟云学术

Development of planar diagnostics for imaging Mach 8 flowfields using carbon dioxide and sodium seeding

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Erbland P.¹,Baumgartner M.²,Yalin A.²,Etz M.²,Muzas B.²,Lempert W.²,Smits A.²,Miles R.²,Erbland P.¹,Baumgartner M.²,Yalin A.²,Etz M.²,Muzas B.²,Lempert W.²,Smits A.²,Miles R.²

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/10.2514/6.1997-154

Reference15 articles.

1. Visualization of the structure of supersonic turbulent boundary layers

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

3. Physical model of the swept shock wave/boundary-layer interaction flowfield

4. Demonstration and characterization of filtered Rayleigh scattering for planar velocity measurements

5. Rayleigh scattering measurements in supersonic facilities

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