Numerical Evaluation of the Effects of Inclusions on Solid Rocket Motor Performance
Author:
Affiliation:
1. University of Bologna, FC 47121 Forlì, Italy
2. Avio S.p.A., 00034 Colleferro, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference23 articles.
1. KallmeyerT.SayerL. H. “Differences Between Actual and Predicted Pressure-Time Histories of Solid Rocket Motors,” AIAA Paper 1982-1094, June 1982. 10.2514/6.1982-1094
2. Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
3. VORTICES IN SOLID PROPELLANT ROCKET MOTORS
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