Aerothermoelastic flutter analysis of variable angle tow composite laminated plates in supersonic flow

Author:

Gong JunqingORCID,Zhang ChuanzengORCID,Xin Fengxian

Funder

Science Fund for Distinguished Young Scholars of Sichuan Province

Universität Siegen

Xi’an Jiaotong University

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Reference39 articles.

1. Historical development of aircraft flutter;Garrick;J. Aircr.,1981

2. Finite-element analysis of the fluttering panels excited by external forces;Surace;J. Sound. Vib.,1999

3. Flutter of a panel supported on an elastic foundation;Chopra;AIAa J.,1975

4. Generalized thermoelastic functionally graded on a thin slim strip Non-Gaussian laser beam;Abo-Dahab;Symmetry (Basel),2020

5. Plane waves in generalized magneto-thermo-viscoelastic medium with voids under the effect of initial stress and laser pulse heating;Othman;Struct. Eng Mech.,2020

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