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Combined mechanical loading of composite tubesAn analytical/experimental investigation was performed to study the effect of material nonlinearities on the response of composite tubes subjected to combined axial and torsional loading. The effect of residual stresses on subsequent mechanical response was included in the investigation. Experiments were performed on P75/934 graphite-epoxy tubes with a stacking sequence of (15/0/ + or - 10/0/ -15), using pure torsion and combined axial/torsional loading. In the presence of residual stresses, the analytical model predicted a reduction in the initial shear modulus. Experimentally, coupling between axial loading and shear strain was observed in laminated tubes under combined loading. The phenomenon was predicted by the nonlinear analytical model. The experimentally observed linear limit of the global shear response was found to correspond to the analytically predicted first ply failure. Further, the failure of the tubes was found to be path dependent above a critical load level.
Document ID
19890003310
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Derstine, Mark S.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Pindera, Marek-Jerzy
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Bowles, David E.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Composite Materials
Report/Patent Number
VPI-E-88-18
NASA-CR-183012
NAS 1.26:183012
CCMS-88-11
Report Number: VPI-E-88-18
Report Number: NASA-CR-183012
Report Number: NAS 1.26:183012
Report Number: CCMS-88-11
Accession Number
89N12681
Funding Number(s)
CONTRACT_GRANT: NAG1-343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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