Turbulent Flow Analysis of Erosive Burning of Cylindrical Composite Solid Propellants
Author:
Affiliation:
1. The Pennsylvania State University, University Park, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference17 articles.
1. 3Razdan, M. K. and Kuo, K. K. "Erosive Burning Study of Composite Solid Propellants by Turbulent Boundary-Layer Approach,'M/A4 Journal, Vol.17, Nov. 1979, pp.1225-1233.
2. Measurements and Model Validation for Composite Propellants Burning under Cross Flow of Gases
3. Reacting Turbulent Boundary-Layer Approach to Solid Propellant Erosive Burning
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