Nonlinear response of composite panels of high speed aircraft-Reference-Cited by-同舟云学术

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Nonlinear response of composite panels of high speed aircraft

Published:1993-01 Issue:7-8 Volume:3 Page:645-660
ISSN:0961-9526
Container-title:Composites Engineering
language:en
Short-container-title:Composites Engineering

Author:

Kavallieratos P.,Vaicaitis R.

Publisher

Elsevier BV

Subject

General Engineering

Reference25 articles.

1. Structural dynamic and aeroelastic considerations for hypersonic vehicles;Cazier,1991

2. Nonlinear response and fatigue of stiffened panels;Choi;Probabilistic Engng Mech,1989

3. Pressure fluctuation inputs and response of panels underlying attached and separated supersonic turbulent boundary layers;Coe;NASA TM X-82,1972

4. Transmission of noise from a turbulent boundary layer through a flexible plate into a closed cavity;Dowell;J. Acoust. Soc. Am,1969

Cited by 6 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. Nonlinear Response of Stiffened Panel Suffered from Thermo-Acoustic Loadings;Applied Mechanics and Materials;2014-11

2. Aerothermoacoustic Response of Shape Memory Alloy Hybrid Composite Panels;Journal of Aircraft;2009-09

3. Thermoacoustic Random Response of Shape Memory Alloy Hybrid Composite Plates;Journal of Aircraft;2008-05

4. Nonlinear response of cylindrical shells to random excitation;Nonlinear Dynamics;1999

5. Prediction of statistical dynamics of thermally buckled composite panels;39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit;1998-04-20

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