Accession Number : AD0673005
Title : TEMPERATURE AND THERMAL STRESS PROBLEMS OF THIN-WALLED SPHERES AND CONES WITH AERODYNAMIC HEATING.
Descriptive Note : Research rept.,
Corporate Author : POLYTECHNIC INST OF BROOKLYN N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS
Personal Author(s) : Chu,Szu Hsiung ; Nardo,S. V. ; Goldberg,M. A.
Report Date : JUL 1968
Pagination or Media Count : 140
Abstract : A number of exact and approximate solutions are presented for the axisymmetrical temperature distribution and thermal stresses in thin spherical, conical and spherically-blunted shells. In the heat conduction analysis, the thermal input is assumed to be in the form of aerodynamic heating. Spherical shell and truncated cone problems with various boundary conditions are solved; also presented are solutions involving a combination of these shell elements, namely, a spherically-blunted cone. Thermal stress solutions are obtained for the foregoing problems. The governing equations assume no coupling between the thermal and elastic fields. J. W. Geckeler's assumptions are used to get the approximate solutions for hemispherical, conical, and combined shell configurations. Both simply-supported and fixed-edge boundary conditions are considered. (Author)
Descriptors : (*SHELLS(STRUCTURAL FORMS), AERODYNAMIC HEATING), THERMAL CONDUCTIVITY, SPHERES, CONICAL BODIES, BLUNT BODIES, THICKNESS, HEAT TRANSFER, MATHEMATICAL ANALYSIS, THERMAL STRESSES
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE