Accession Number : ADA133364
Title : Propellant Nonlinear Constitutive Theory Extension: Preliminary Results.
Descriptive Note : Special technical rept. Sep 80-Sep 82 on Phases 1, 2, and 3,
Corporate Author : UNITED TECHNOLOGIES CORP SUNNYVALE CA CHEMICAL SYSTEMS DIV
Personal Author(s) : Francis,E C ; Lemini,D G ; Carlton,C ; Huffered,W L ; Gurtin,M
PDF Url : ADA133364
Report Date : Aug 1983
Pagination or Media Count : 338
Abstract : This report details the technical effort put forth by CSD and its subcontractors during the first three phases of this program for propellant nonlinear constitutive theory extension. This includes the Phase I preliminary study in which the Quinlah theory was critiqued, alternate approaches were studied and detailed research planning accomplished. Also included are the detailed experimental evaluations of propellant during Phases II and III, the uniaxial/isothermal investigation and the two-dimensional variable temperature investigation. Detailed subcontractor theoretical development and predictions are presented.
Descriptors : *Solid rocket propellants, *Thermomechanics, *Nonlinear analysis, Theory, Mathematical models, Stress strain relations, Loads(Forces), Viscoelasticity, Temperature, Two dimensional, Three dimensional, Isotherms
Subject Categories : Numerical Mathematics
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE