Research Article
Analytical Solution for a Multi-layer Thick Cylindrical Shell Subjected to Axial Inertia Applicable for Slump Estimations of Solid Propellant Rocket Motor Grains
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