Effect of surface reactions on the solid propellant response function.
Author:
Affiliation:
1. Stanford Research Institute, Menlo Park, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4522
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4. Stewartson, K., The Theory of Laminar Boundary Layers in Compressible Fluids, Clarendon, Oxford, England, 1964, Chap. 3, pp.37-41.
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