Nonlinear response and fatigue of stiffened panels-Reference-Cited by-同舟云学术

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Nonlinear response and fatigue of stiffened panels

Published:1989-09 Issue:3 Volume:4 Page:150-160
ISSN:0266-8920
Container-title:Probabilistic Engineering Mechanics
language:en
Short-container-title:Probabilistic Engineering Mechanics

Author:

Choi Siu-Tong,Vaicaitis Rimas

Publisher

Elsevier BV

Subject

Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Condensed Matter Physics,Nuclear Energy and Engineering,Civil and Structural Engineering,Statistical and Nonlinear Physics

Reference49 articles.

1. National aero-space plane: technology for America's future;Williams;Aerospace America,1986

2. Acoustic fatigue: overview of activities at NASA Langley;Mixon;NASA TM-89143,1987

3. Nonlinear random response of composite panels;Mei;NASA CR-176689,1985

4. Nonlinear multimode response of clamped rectangular plates to acoustic loading;Mei;AIAA Journal,1986

5. Advanced composite joints: design and acoustic fatigue characteristics;Jacobson,1972

Cited by 4 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. Prediction of the Dynamic Response and Fatigue Life of Panels Subjected to Thermo-Acoustic Loading;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19

2. Nonlinear Models for Double-Wall Systems for Vibrations and Noise Control;Journal of Aircraft;1997-11

3. Nonlinear response and sonic fatigue of National Aerospace Space Plane surface panels;Journal of Aircraft;1994-01

4. Nonlinear response of composite panels of high speed aircraft;Composites Engineering;1993-01

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