An Investigation of High-Cycle Fatigue Models for Metallic Structures Exhibiting Snap-Through Response-Reference-Cited by-同舟云学术

An Investigation of High-Cycle Fatigue Models for Metallic Structures Exhibiting Snap-Through Response

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Przekop Adam¹,Rizzi Stephen²,Sweitzer Karl³

Affiliation:

1. National Institute of Aerospace

2. NASA Langley Research Center

3. ITT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2204

Reference14 articles.

1. 1Mei, C., Dhainaut, J.M., Duan, B., Spottswood, S.M., and Wolfe, H.F. "Nonlinear random response of composite panels in an elevatedthermal environment,"Air Force Research Laboratory AFRL-VA-WP-TR-2000-3049,WPAFB, OH, 2000.

2. Experimental snap-through boundaries for acoustically excited, thermally buckled plates

3. Nonlinear and snap-through responses of curved panels to intense acoustic excitation

4. High-intensity acoustic tests of a thermally stressed plate

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3. Detecting Snap-Through Boundaries Using an Adaptive Parameter Space Approach;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

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