Surface recession rate of an ablating polymer.
Author:
Affiliation:
1. Avco Everett Research Laboratory, Everett, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4870
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1. Boundarv-Layer Stability and Transition in Subsonic and Supersonic Flow
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