Orbiter BLT Flight Experiment Wind Tunnel Simulations: Nearfield Flowfield Imaging and Surface Thermography-Reference-Cited by-同舟云学术

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Orbiter BLT Flight Experiment Wind Tunnel Simulations: Nearfield Flowfield Imaging and Surface Thermography

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Danehy Paul¹,Ivey Christopher²,Bathel Brett³,Inman Jennifer¹,Jones Stephen¹,Jiang Naibo⁴,Webster Matt⁴,Lempert Walter⁴,Miller Joseph⁵,Meyer Terry⁵,Watkins A. N.¹,Goodman K Z.¹

Affiliation:

1. NASA Langley Research Center

2. Johns Hopkins University

3. University of Virginia

4. Ohio State University

5. Iowa State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1571

Reference27 articles.

1. C. H. Campbell, M. T. Garske, J. Kinder, and S. A. Berry, "Orbiter Entry Boundary Layer Flight Testing," AIAA PaperNumber2008-635,46thAIAAAerospaceSciencesMeetingandExhibit,7-10January2008,Reno,Nevada.

2. B. P. Anderson, C. H. Campbell, L. A. Saucedo, G. R. Kinder, "BLT Flight Experiment Overview and In- Situ Measurements" AIAA-2010-0240,48thAIAAAerospaceSciencesMeeting,Orlando,FL,January,2010.

3. Effects of Roughness on Hypersonic Boundary-Layer Transition

4. T.J.Horvath,D.M.Tomek,K.T.Berger,S.C.Splinter,J.N.Zalameda,P.W.Krasa,S.Tack,R.J.Schwartz,D.M. Gibson, and A. B. Tietjen, "The HYTHIRM Project: Flight Thermography of the Space Shuttle during Hypersonic Reentry,"AIAAPaper2010-241,Jan.2010.

5. Transition Induced by Fence Geometries on Shuttle Orbiter at Mach 10

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