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Optical methods of stress analysis applied to cracked componentsAfter briefly describing the principles of frozen stress photoelastic and moire interferometric analyses, and the corresponding algorithms for converting optical data from each method into stress intensity factors (SIF), the methods are applied to the determination of crack shapes, SIF determination, crack closure displacement fields, and pre-crack damage mechanisms in typical aircraft component configurations.
Document ID
19930061801
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Smith, C. W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Structural integrity of aging airplanes (A93-45772 19-01)
Publisher: Springer-Verlag
Subject Category
Structural Mechanics
Accession Number
93A45798
Distribution Limits
Public
Copyright
Other

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