K. Renganathan
Structural Analysis and Testing Group, Vikram Sarabhai Space Centre
Trivaudrurn-695022, India
B. Nageswara Rao
Structural Analysis and Testing Group, Vikram Sarabhai Space Centre
Trivaudrurn-695022, India
M.K. Jana
Structural Analysis and Testing Group, Vikram Sarabhai Space Centre
Trivaudrurn-695022, India
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How to cite this article
K. Renganathan, B. Nageswara Rao and M.K. Jana, 2006. Analytical Solution for a Multi-layer Thick Cylindrical Shell Subjected to Axial Inertia Applicable for Slump Estimations of Solid Propellant Rocket Motor Grains. Trends in Applied Sciences Research, 1: 123-131.
URL: https://scialert.net/abstract/?doi=tasr.2006.123.131
URL: https://scialert.net/abstract/?doi=tasr.2006.123.131