Quasi-Static Thermal Stresses in a Robin’s Thin Hollow Cylinder with Internal Moving Heat Source

Abstract

2.Introduction: During the second half of 20 th century, non-isothermal problems of the theory of elasticity became increasingly important. This is due to their wide application in diverse fields. The high velocities of modern aircraft give rise to aerodynamic heating, which produces intense thermal stresses that reduce the strength of aircraft structure. Recently D. T. Solanke, M. H. Durge have studied the thermal stresses in thin cylinder with Dirichlet's, Neumann's, Robin's boundary condition and in thin hollow cylinder with Dirichlet's, Neumann's boundary condition. Now authors in this present paper determine temperature, thermal stresses, in thin hollow cylinder with Robis's boundary condition, determined by

Three-Dimensional Unsteady State Temperature Distribution of Thin Rectangular Plate with Moving Point Heat Source

“…Temperature distribution, thermal functions, and displacement at any point of semi-infinite rectangular slab with internal heat source using integral transform technique are solved by [7]. Using integral transform technique and Green's theorem [8] has determined temperature distribution and thermal stresses by taking second kind boundary condition in thin rectangular plate with moving line heat source. Reference [9] has determined thermal stresses on thin rectangular plate by integral transform with internal moving point heat source.…”