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090			_aB-20736
245	1	0	_aStress and failure analysis of a pin-loaded composite plate: an experimental study
490	0		_vJournal of Composite Materials, 24(10), p.1101-1120, 1990
520	3		_aA graphite/epoxy quasi-isotropic composite plate was loaded through an aluminum pin. High-sensitivity moire interferometry was used to obtain fringe patterns of in-plane displacement components near the pin-plate contact surface. Stresses around and near the contact surface were determined from the experimentally obtained displacements using a localized hybrid approach which consisted of introducing the displacements around a local region of interest into a finite element analysis. X-ray radiography and optical microscopy were employed in a failure analysis of the plate. Stress distributions on the near contact interface were obtained. Local damage was also documented successfully. A simple failure prediction based on classical laminate theory gave good agreement with the observed location of damage. Valuable local aspects fric tional phenomena were documented.
700	1	2	_aTsai, M. Y.
700	1	2	_aMorton, J.
856	4	0	_uhttps://drive.google.com/file/d/1zYVPM04RSLijZQ5xMNsmNlKRTOCeUm_X/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx
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