APPLICATIONS OF NON-LINEAR VISCOELASTICITY AND CUMULATIVE DAMAGE (A REALISTIC EVALUATION OF REAL PROPELLANT BEHAVIOR)
Abstract
A study was undertaken to provide a realistic evaluation of real propellant behaviors, with emphasis upon the effects of larger strains and their attendant marked nonlinear viscoelastic behavior. To accomplish this primary objective, efforts were made to: (1) evaluate the nonlinear viscoelastic response properties of solid propellants in terms of the theories of Farris, and reduce to practice the associated analytical methods; and (2) develop a practical, empirical method of calculating cumulative damage in terms of a strain failure criterion.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1970
- Accession Number
- AD0710776
Entities
People
- Kenneth W. Bills Jr.
- Leonard R. Herrmann
Organizations
- Aerojet Rocketdyne Holdings