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Evaluation of the Behavior of Technova Corporation Rod-Stiffened Stitched Compression SpecimensUnder Space Act Agreement 1347 between NASA and Technova Corporation, Technova designed and fabricated two carbon-epoxy crippling specimens and NASA loaded them to failure in axial compression. Each specimen contained a pultruded rod stiffener which was held to the specimen skin with through-the-thickness stitches. One of these specimens was designed to be nominally the same as pultruded rod stitched specimens fabricated by Boeing under previous programs. In the other specimen, the rod was prestressed in a Technova manufacturing process to increase its ability to carrying compressive loading. Experimental results demonstrated that the specimen without prestressing carried approximately the same load as the similar Boeing specimens and that the specimen with prestressing carried significantly more load than the specimen without prestressing.
Document ID
20140002900
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Jegley, Dawn C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 14, 2014
Publication Date
October 1, 2013
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2013-218049
NF1676L-17471
L-20331
Funding Number(s)
WBS: WBS 031102.02.07.11.8922.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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