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NASA NTRS ยท 19790010870

High temperature strain gage evaluation

Abstract

The structural thermal test of an advanced ramjet missile section required strain measurements as high as 922 K (1200 F). Since there is relatively little experience in the use of strain gages above the 700-755 K (800-900 F) level, a program was initiated to select and evaluate the best available gage. Candidate gages suitable for measurements up to 922 K (1200 F) were selected. This involved the determination of their operating characteristics, availability, cost, installation aspects, etc. The evaluation involved the following tests: strain as a function of load at room temperature and apparent strain as a function of temperature.

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BibTeXRIS

Gonzalez, J. I.. 1977-01-01. High temperature strain gage evaluation. https://ntrs.nasa.gov/citations/19790010870

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