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Shear-Panel Test Fixture Eliminates Corner StressesNew design eliminates corner stresses while maintaining uniform stress across panel. Shear panel test fixture includes eight frames and eight corner pins. Fixture assembled in two halves with shear panel sandwiched in between. Results generated from this fixture will result in good data base for design of efficient aircraft structures and other applications.
Document ID
19830000383
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kiss, J. J. (Army Aviation Research and Development Command)
Farley, G. L. (Army Aviation Research and Development Command)
Baker, D. J.
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12930
Accession Number
83B10383
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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