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Thermal Output of WK-Type Strain Gauges on Various Materials at Cryogenic and Elevated TemperaturesStrain gage apparent strain (thermal output) is one of the largest sources of error associated with the measurement of strain when temperatures and mechanical loads are varied. In this paper, experimentally determined apparent strains of WK-type strain gages, installed on both metallic and composite-laminate materials of various lay-ups and resin systems for temperatures ranging from -450 F to 230 F are presented. For the composite materials apparent strain in both the 0 ply orientation angle and the 90 ply orientation angle were measured. Metal specimens tested included: aluminum-lithium alloy (Al-LI 2195-T87), aluminum alloy (Al 2219-T87), and titanium alloy. Composite materials tested include: graphite-toughened-epoxy (IM7/997- 2), graphite-bismaleimide (IM7/5260), and graphite-K3 (IM7/K3B). The experimentally determined apparent strain data are curve fit with a fourth-order polynomial for each of the materials studied. The apparent strain data and the polynomials that are fit to the data are compared with those produced by the strain gage manufacturer, and the results and comparisons are presented. Unacceptably high errors between the manufacture's data and the experimentally determined data were observed (especially at temperatures below - 270-F).
Document ID
19990009541
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kowalkowski, Matthew K.
(NASA Langley Research Center Hampton, VA United States)
Rivers, H. Kevin
(NASA Langley Research Center Hampton, VA United States)
Smith, Russell W.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1998
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
L-17752
NAS 1.15:208739
NASA/TM-1998-208739
Funding Number(s)
PROJECT: RTOP 242-33-01-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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