A SIMPLIFIED METHOD FOR DYNAMIC STRESS ANALYSIS OF AXIALLY SYMMETRIC SOLID PROPELLANT GRAINS.

Abstract

The report investigates the response to transient axially symmetric end pressure of a finite length hollow circular cylinder with a fixed outer surface. Axially symmetric thickness shear motion is assumed predominant and a correspondingly simplified equation of motion is derived. It is found that, for forced motion problems, considerable simplification is obtained if, instead of solving the equations of motion exactly, one uses Galerkin's method. One- and two-term' Galerkin expansions are compared with exact solutions for free vibrations and for transient response to suddenly applied pressure. Agreement is good for the one-term expansion and excellent for the two-term expansion. The equations are derived for a standard linear solid as well as an elastic grain, calculations are performed for the elastic grain only. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1965
Accession Number
AD0475768

Entities

People

  • James S. Whittier
  • John Paul Jones

Organizations

  • The Aerospace Corporation

Tags

DTIC Thesaurus Topics

  • Agreements
  • Energetic Materials
  • Equations
  • Equations Of Motion
  • Materials
  • Mathematics
  • Propellant Grains
  • Propellants
  • Solid Propellants
  • Standards
  • Stress Analysis
  • Stresses
  • Thickness

Readers

  • Rocket Propulsion.
  • Structural Dynamics.