Thickening of optimally selected locations on panels subjected to unyawed flow for substantial delay of the panel flutter-Reference-Cited by-同舟云学术

Thickening of optimally selected locations on panels subjected to unyawed flow for substantial delay of the panel flutter

Published:2020-12 Issue:6 Volume:59 Page:5031-5044
ISSN:1110-0168
Container-title:Alexandria Engineering Journal
language:en
Short-container-title:Alexandria Engineering Journal

Author:

M.Y.B. Elshabasy Mohamed,Kouritem Sallam A.

Publisher

Elsevier BV

Subject

General Engineering

Reference41 articles.

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2. Finite element flutter analysis of laminated composite panels;Chowdary;Comput. Struct.,1994

3. Review of nonlinear panel flutter at supersonic and hypersonic speeds;Mei;Appl. Mech. Rev.,1999

4. Flutter control of a composite plate with piezoelectric multilayered actuators;Raja;Aerosp. Sci. Technol.,2006

5. Finite element time domain – modal formulation for nonlinear flutter of composite panels;Zhou;AIAA J.,1995

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