A model of the effects of pressure and crossflow velocity on composite propellant burning rate
Author:
Affiliation:
1. California, University, Los Alamos, N. Mex.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1171
Reference23 articles.
1. A model of erosive burning of composite propellants
2. Erosive burning of composite solid propellants - Experimental and modeling studies
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