Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. B. F. Goodrich Aerospace, Chula Vista, California 91910
3. NASA Johnson Space Flight Center, Houston, Texas 77058
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3327
Reference15 articles.
1. Langley hypersonic aerodynamic/aerothermodynamic testing capabilities - Present and future
2. Surface temperature/heat transfer measurement using a quantitative phosphor thermography system
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