Progress in the simulation of particulate interactions in solid propellant rocket exhausts
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc., Dublin, PA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3590
Reference30 articles.
1. Analysis of two-phase flow processes in rocket exhaust plumes
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