Infrared Sensing Aeroheating Flight Experiment: STS-96 Flight Results-Reference-Cited by-同舟云学术

Infrared Sensing Aeroheating Flight Experiment: STS-96 Flight Results

Published:2001-07 Issue:4 Volume:38 Page:465-472
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Blanchard Robert C.,Wilmoth Richard G.,Glass Christopher E.,Merski N. Ronald,Berry Scott A.,Bozung Timothy J.¹,Tietjen Alan,Wendt Jodean,Dawson Donald

Affiliation:

1. George Washington University, Hampton, Virginia 23681-2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3713

Reference11 articles.

1. X-33 hypersonic boundary layer transition

2. Bouslog, S. A., An, M. Y., and Derry, S. M. “Orbiter Windward-Surface Boundary-Layer Transition Flight Data,” edited by D. A. Throckmorton,NASACP-3248,Pt. 2,1995, pp.703-739.

3. Shuttle Boundary-Layer Transition Due to Distributed Roughness and Surface Cooling

4. Hypersonic boundary layer transition for X-33 Phase II vehicle

5. X-33 experimental aeroheating at Mach 6 using phosphor thermography

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