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Thin-walled composite beams under bending, torsional, and extensional loadsSymmetric and antisymmetric layup graphite-epoxy composite beams with thin-walled rectangular cross sections are fabricated using an autoclave molding technique and tested under bending, torsional, and extensional loads. The bending slope and elastic twist at a station are measured using an optical system, and the results correlated with predicted values from a simple beam analysis as well as a refined finite element analysis. A symmetric ply layup results in bending-twist coupling whereas an antisymmetric layup causes extension-twist coupling. Simple analytical results with plane-stress assumption agree better with measured data as well as finite element predictions than with plane-strain assumption. For symmetric layup beams, the bending-induced twist and torsion-induced bending slope are predicted satisfactorily using simple analytical solution. Correlations with measured data, however, are generally improved using a finite element solution. For antisymmetric beams, axial force-induced twist is predicted satisfactorily by both methods.
Document ID
19900057677
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chandra, Ramesh
(Maryland Univ. College Park, MD, United States)
Stemple, Alan D.
(Maryland Univ. College Park, MD, United States)
Chopra, Inderjit
(Maryland, University College Park, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Publication Information
Publication: Journal of Aircraft
Volume: 27
ISSN: 0021-8669
Subject Category
Structural Mechanics
Accession Number
90A44732
Funding Number(s)
CONTRACT_GRANT: NAG1-853
Distribution Limits
Public
Copyright
Other

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