Development of efficient finite elements for structural integrity analysis of solid rocket motor propellant grains
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Reference42 articles.
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4. Analytical solution for a multi-layer thick cylindrical shell subjected to axial inertia applicable for slump estimates of solid propellant rocket motor grains;Renganathan;Trends in Applied Science Research,2006
5. Finite element analysis, design and experiment on solid propellant motors with stress reliever;Chen;Finite Elements in Analysis and Design,1998
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