NDLI: Prediction of response of aircraft panels subjected to acoustic and thermal loads

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Prediction of response of aircraft panels subjected to acoustic and thermal loads

Content Provider	NASA Technical Reports Server (NTRS)
Author	Mei, Chuh
Copyright Year	1992
Description	The primary effort of this research project has been focused on the development of analytical methods for the prediction of random response of structural panels subjected to combined and intense acoustic and thermal loads. The accomplishments on various acoustic fatigue research activities are described first, then followed by publications and theses. Topics covered include: transverse shear deformation; finite element models of vibrating composite laminates; large deflection vibration modeling; finite element analysis of thermal buckling; and prediction of three dimensional duct using boundary element method.
File Size	1234103
Page Count	48
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19920015102
Archival Resource Key	ark:/13960/t48q0xq82
Language	English
Publisher Date	1992-05-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Panels Shear Acoustic Fatigue Ducts Free Vibration Forced Vibration Laminates Finite Element Method Acoustic Excitation Thermal Buckling Composite Structures Aircraft Structures Random Vibration Boundary Element Method Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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