Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations
Author:
Affiliation:
1. Department of Aerospace Engineering, Ryerson University, 350 Victoria St., Toronto, Ontario, Canada M5B 2K3
Abstract
Publisher
Hindawi Limited
Subject
Aerospace Engineering
Link
http://downloads.hindawi.com/journals/ijae/2008/826070.pdf
Reference20 articles.
1. Progress in Astronautics and Aeronautics,1992
2. Numerical model for pellet-dispersion igniter systems
3. Nonsteady burning phenomena of solid propellants - Theory and experiments.
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