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Numerical calibration of the stable poisson loaded specimenAn analytical calibration of the Stable Poisson Loaded (SPL) specimen is presented. The specimen configuration is similar to the ASTM E-561 compact-tension specimen with displacement controlled wedge loading used for R-Curve determination. The crack mouth opening displacements (CMOD's) are produced by the diametral expansion of an axially compressed cylindrical pin located in the wake of a machined notch. Due to the unusual loading configuration, a three-dimensional finite element analysis was performed with gap elements simulating the contact between the pin and specimen. In this report, stress intensity factors, CMOD's, and crack displacement profiles are reported for different crack lengths and different contacting conditions. It was concluded that the computed stress intensity factor decreases sharply with increasing crack length, thus making the SPL specimen configuration attractive for fracture testing of brittle, high modulus materials.
Document ID
19930003550
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ghosn, Louis J.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Calomino, Anthony M.
(NASA Lewis Research Center Cleveland, OH, United States)
Brewer, Dave N.
(Army Aviation Systems Command Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:105609
E-7335
NASA-TM-105609
Report Number: NAS 1.15:105609
Report Number: E-7335
Report Number: NASA-TM-105609
Accession Number
93N12738
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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