Analysis of the Chemically Reacting Laminar Boundary Layer during Hybrid Combustion
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign, III.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50671
Reference18 articles.
1. Introductory Considerations on Hybrid Rocket Combustion
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