Approximate Three-Dimensional Solutions for Transient Temperature Distribution in Shells of Revolution

Author:

BRULL MAURICE A.1,VINSON JACK R.2

Affiliation:

1. University of Pennsylvania,

2. General Electric Company,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference4 articles.

1. New Methods in Heat Flow Analysis With Application to Flight Structures

2. Morse, P. M., and Feshbach, H., Methods of Theoretical Physics, Part 1, Chapter 5, pp.495-562; McGraw-Hill Book Co., Inc., New York, 1953.

3. Churchill, R. V., Fourier Series and Boundary Value Problems, Chapter 3, Sec. 24-25, pp.47-52; McGraw-Hill Book Co., Inc., New York,1941.

4. Carslaw, H. S., and Jaeger, J. C , Conduction of Heat in Solids•, Chapter 1, Sec. 11, pp.22-24; Oxford Press, England,1947.

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1. Thermoelastic Effects on Shells;The Behavior of Shells Composed of Isotropic and Composite Materials;1993

2. Steady‐State Nonlinear Heat Transfer in Multilayered Composite Panels;Journal of Engineering Mechanics;1992-08

3. Steady-state heat conduction in multilayered composite plates and shells;Computers & Structures;1991-01

4. Heat conduction in plates and shells with emphasis on a conical shell;International Journal of Solids and Structures;1986

5. BIBLIOGRAPHY;Thermoelasticity;1986

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