Flutter analysis of cantilevered curved composite panels-Reference-Cited by-同舟云学术

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Flutter analysis of cantilevered curved composite panels

Published:1993-01 Issue:1-4 Volume:25 Page:89-93
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Pidaparti R.M.V.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference21 articles.

1. The Theory of Aeroelasticity;Fung,1955

2. Principles of Aeroelasticity;Bisplinghoff,1962

3. Aeroelasticity of Plates and Shells;Dowell,1975

4. A Modern Course in Aeroelasticity;Dowell,1978

5. Some recent contributions to panel flutter research;Fung;AIAA J.,1963

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow;Acta Mechanica;2023-09-10

2. Finite element analysis of the panel flutter of stiffened shallow shells;Continuum Mechanics and Thermodynamics;2022-08-01

3. Flutter characteristics of multi-layered composite shell panels under supersonic flow with curvature effect;Waves in Random and Complex Media;2022-06-09

4. Thickening of optimally selected locations on panels subjected to unyawed flow for substantial delay of the panel flutter;Alexandria Engineering Journal;2020-12

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

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