Structural vibration considerations for solid rocket internal ballistics modeling
Author:
Affiliation:
1. Toronto, Univ., Canada
2. Defence Research Establishment Valcartier, Val-Belair, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3804
Reference17 articles.
1. Greatrix, D.R. "Combined Structural Oscillation Effects onSolid Rocket InternalBallistics,"AIAA PaperNo.99-2509, June 1999.
2. Harris, P.O.,Wong, F.C.,and de Champlain, A. "The Influence of Structural Vibrations onPulse-Triggered Nonlinear Instability in Solid Rocket Motors:AnExperimentalStudy,"AIAAPaperNo. 96-3250,July 1996.
3. Experimental Database Describing Pulse-Triggered Nonlinear Instability in Solid Rocket Motors
4. Elements of modelling the use of particles in solid-propellant rocket motors
5. Solutions in the large for nonlinear hyperbolic systems of equations
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