DNS and LES computations of model solid rocket motors
Author:
Affiliation:
1. Illinois, Univ., Urbana
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3571
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1. Computations of two-phase flow in aluminized solid propellant rockets
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5. 5Williams, F. A., Barrere, M., and Huang, N. C., Fundamental Aspects of Solid Propellant Rockets, NATO AGARDograph, No. 116,1969.
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