Nonlinear response and sonic fatigue of metal and composite panels-Reference-Cited by-同舟云学术

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Nonlinear response and sonic fatigue of metal and composite panels

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:13th Aeroacoustics Conference
language:
Short-container-title:

Author:

VAICAITIS RIMAS¹,ARNOLD ROCKY²

Affiliation:

1. Columbia University, New York

2. Anamet Laboratories, Inc., Hayward, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3938

Reference73 articles.

1. Acoustic Fatigue Characteristics." AFFDL-TR-71-126.

2. Air Force Base, Ohia, 1972.

3. 80-3019, Air Force Wright Aeronautical Laboratories,

4. Wright-Patterson Air Force Base. Ohio, April 1980.

5. Soovere, J. "Effect of Acoustic, Thermal and Shear Loading on Flat Integrally Stiffened GraphiteEpoxy Fuselage Panels, NADC-78169-60, 1982.

Cited by 2 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. Finite element nonlinear random response of composite plates to acoustic and thermal loads applied simultaneously;36th Structures, Structural Dynamics and Materials Conference;1995-04-10

2. Nonlinear Response and Sonic Fatigue of High Speed Aircraft;Computational Stochastic Mechanics;1991

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