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Suggested Procedures for Installing Strain Gauges on Langley Research Center Wind Tunnel Balances, Custom Force Measuring Transducers, Metallic and Composite Structural Test ArticlesThe character of force and strain measurement testing at LaRC is such that the types of strain gauge installations, the materials upon which the strain gauges are applied, and the test environments encountered, require many varied approaches. In 1997, a NASA Technical Memorandum (NASA TM 110327) was generated to provide the strain gauge application specialist with a listing of recommended procedures for strain gauging various transducers and test articles at LaRC. The technical memorandum offered here is an effort to keep the strain gauge user informed of new technological enhancements in strain-gauging methodology while preserving the strain-gauging guidelines set forth in the 1997 TM. This document provides detailed recommendations for strain gauging LaRC-designed balances and custom transducers, composite materials, cryogenic and high-temperature test articles, and selected non-typical or unique materials or test conditions. Additionally, one section offers details for installing Bragg-Grating type fiber-optic strain sensors for non-typical test scenarios.
Document ID
20040075552
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Moore, Thomas C., Sr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
May 1, 2004
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-2004-213017
L-19020
Report Number: NASA/TM-2004-213017
Report Number: L-19020
Funding Number(s)
OTHER: 23-761-20-5H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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