Improved Time-Dependent Flowfield Solution for Solid Rocket Motors
Author:
Affiliation:
1. Marquette University, Milwaukee, Wisconsin 53233
2. University of Utah, Salt Lake City, Utah 84112
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7507
Reference20 articles.
1. Acoustic boundary layers in solid propellant rocket motors using Navier-Stokes equations
2. Numerical study of the unsteady flow in a simulated solid rocket motor
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