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The strain-gage method for obtaining airplane structural load measurements
Atnip, F.K.
Atnip, F.K.
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t1960_Atnip.pdf
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1960-05
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Thesis
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Electronic dissertations
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Abstract
It was the purpose of this thesis to
present the development of the strain-gage calibration theory using calculus
notation. The development or the theory using matrix notation is
included for comparative purposes. To provide continuity in the discussion
of the strain-gage method for obtaining structural load measurements,
the procedure for converting the in-flight recorded loads to net
loads and air loads is presented in Appendix A.
Table of Contents
Problem and scope -- Review of the literature -- Theory -- Applications of the theory -- Summary and cunclusions -- Bibliography -- Appendix
Description
Thesis (M.S.)-- University of Wichita, College of Engineering, Dept. of Mechanical Engineering
Publisher
Wichita State University
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Wichita State University