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End Restraints for Impact-Energy-Absorbing Tube SpecimensInexpensive device developed that eliminates tipping problem without affecting crushing process. Device consists of soft sponge-rubber insert approximately 0.5 inches (1.3 centimeters) thick, cut to same diameter as internal diameter of tube specimen. Metal washer, slightly smaller than internal diameter of tube, placed on top of rubber insert. Screw passed through washer and rubber insert and threaded into base of test machine. As screw tightened against washer, rubber insert compressed and expands radially. Radial expansion applies pressure against internal wall of tube specimen, which provides sufficient support to tube to prevent tipping.
Document ID
19850000218
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Farley, G. L.
(Structures Laboratory, U.S. Army Research and Technology Laboratories, AVSCOM)
Modlin, J. T.
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13179
Accession Number
85B10218
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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