
Accession Number : AD0664767
Title : ANALYTICAL SOLUTION OF THERMAL STRESSES FOR A VISCOELASTIC HOLLOW CYLINDER.
Corporate Author : ILLINOIS UNIV URBANA COORDINATED SCIENCE LAB
Personal Author(s) : Hsu,John
Report Date : JAN 1968
Pagination or Media Count : 48
Abstract : A solution is presented for the thermal stresses in an isotropic, homogeneous, viscoelastic, hollow cylinder enclosed by a rigid casing. The governing equation, which is of the integraldifferential form, is integrated numerically. The resulting partial differential equation is solved exactly subjected to the imposed boundary conditions. For comparison, a simple fourparameter viscoelastic material is chosen since an independent analytical solution is available. A second example is presented in order to demonstrate the capability of this solution in handling large numbers of viscoelastic parameters which are usually required to characterize real solid propellant and other polymeric structural materials. (Author)
Descriptors : (*CYLINDRICAL BODIES, *THERMAL STRESSES), (*ROCKET ENGINE CASES, STRUCTURAL PROPERTIES), SOLID ROCKET PROPELLANTS, PARTIAL DIFFERENTIAL EQUATIONS, BOUNDARY VALUE PROBLEMS, EXPONENTIAL FUNCTIONS, SERIES(MATHEMATICS), NUMERICAL ANALYSIS, VISCOELASTICITY, SHELLS(STRUCTURAL FORMS), STRAIN(MECHANICS), TEMPERATURE, THESES
Subject Categories : Rockets
Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE