A multicomponent boundary layer chemically coupled to an ablating surface.
Author:
Affiliation:
1. Aerotherm Corporation, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4138
Reference16 articles.
1. Sublimation of graphite at hypersonic speeds
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