Displacement and strain histograms of thermally buckled composite plates in random vibration
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1347
Reference19 articles.
1. Lee,J.,Large-Amplitude Plate Vibration inan Elevated Thermal Environment,WL-TR-92-3049, WrightLaboratory,Wright-PattersonAFB,OH,June, 1992.
2. Sonic fatigue of advanced composite panels in thermal environments
3. Seide,P. and Adami,C.,Dynamic Stability of Beams ina Combined Thermal-Acoustic Environment, AFWAL-TR-83-3072,FlightDynamicLaboratory, Wright-Patterson AFB,OH, 1983.
4. Nonlinear and snap-through responses of curved panels to intense acoustic excitation
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