Closed form solutions – Analysis and optimal design of supersonic composite laminated flat plates considering mechanical and thermal effects-Reference-Cited by-同舟云学术

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Closed form solutions – Analysis and optimal design of supersonic composite laminated flat plates considering mechanical and thermal effects

Published:2019-12 Issue: Volume:230 Page:111491
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Muc A.,Flis J.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference34 articles.

1. Nonconservative problems of the theory of elastic stability;Bolotin,1961

2. On the flutter of panels at high mach numbers, readers' forum;Hedgepeth;J. Aerospace Sci.,1956

3. A study of several aerothermoelastic problems of aircraft structures in high speed flight;Houbolt,1958

4. Inzhenerny Zbornyk;Bolotin,1960

5. Flutter of infinitely long plates and shells, part II: cylindrical shells;Dowell;AIAA J,1966

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2. Aeroelastic-electric flutter characteristics of functionally graded piezoelectric material plates in supersonic airflow;Archive of Applied Mechanics;2024-05-06

3. Comments and remarks on symmetry and asymmetry problems in the design of plated/shell composite structures–Laminates, nanostructures and functionally graded materials;Composites Part C: Open Access;2024-03

4. On concurrent multiscale topology optimization for porous structures under hygro‐thermo‐elastic multiphysics with considering evaporation;International Journal for Numerical Methods in Engineering;2023-04-11

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