Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket Motors
Author:
Affiliation:
1. Michelson Laboratory, Lake, U. S. Naval Ordnance Test Station, Inyokern, China Lake, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.4600
Reference9 articles.
1. Characteristics of the rocket motor unit based on the theory of perfect gases
2. "Foundations of Aerodynamics," byA. M. Keuthe and J. D. Schetzer, John Wiley and Sons, Inc., New York,1950, pp.127-151.
3. On the Steady Flow of a Gas Through a Tube with Heat Exchange or Chemical Reaction
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