Measurements of the total surface emittance of charring ablators.
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference19 articles.
1. Prediction of incipient separation in shock- boundary-layer interactions.
2. Needham, D. A. "Laminar separation in hypersonic flow," Ph.D. thesis,Univ. of London (1965).
3. Mach 8 to 22 studies of flow separations due to deflected control surfaces
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