Effect of aerodynamic heating on deformation of composite cylindrical panels in a gas flow-Reference-Cited by-同舟云学术

Effect of aerodynamic heating on deformation of composite cylindrical panels in a gas flow

Published:1990-01 Issue:3 Volume:15 Page:259-273
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Birman Victor,Bert Charles W.,Elishakoff Isaac

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference17 articles.

1. General Theory of Anisotropic Shells;Ambartsumian,1974

2. Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures;Librescu,1975

3. Design of composite cylindrical shells of minimum weight in supersonic gas flow;Kosichenko;Soviet Aeronautics,1980

4. Experimental investigation at Mach number 3·0 of effects of thermal stresses and buckling on flutter characteristics of flat single-bay panels of length-width ratio 0·96;Dixon;NASA TN D-1485,1962

5. A survey of aerothermoelasticity;Garrick;Aerospace Engng,1963

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4. Supersonic flutter characteristics of composite cylindrical panels;Composite Structures;2008-01

5. PUBLICATIONS ON THERMAL STRESSES;Journal of Thermal Stresses;1991-01