TEMPERATURES AND THERMAL STRESSES IN THIN-WALLED SPHERICAL SEGMENTS.
POLYTECHNIC INST OF BROOKLYN N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS
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The thermal stresses induced in thin-walled spherical shell seqments, subject to a uniform aerodynamic heat input are presented. The problem is divided into two main sections determination of the transient and steady-state temperature distribution in the spherical shell segment, and calculation of the resulting thermal stresses. Author