Analysis was made of stress and displacements in elastic solid propellant grain perforated internally by star shaped configuration, bonded peripherally to elastic motor case and loaded internally by pressure normal to perforation; analysis was performed under assumption of plane strain using conformal mapping and complex variable method of N.I. Muskhelishvili; analysis can be generalized to n-pointed configuration.
Stresses owing to internal pressure in solid propellant rocket grains
ARS J
ARS Journal ; 31 , n 3
1961
9 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Additive Manufacturing of Solid Rocket Propellant Grains
AIAA | 2018
|Modular Dissected Cryogenic Solid-Rocket Propellant Grains
British Library Conference Proceedings | 1998
|Modular Dissected Cryogenic Solid-Rocket Propellant Grains
Online Contents | 2002
|Strain analysis of solid propellant rocket grains
Engineering Index Backfile | 1960
|