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A comparison of the theoretical and experimental frequency- response functions for the B-47 airplane
Dempster, John Benton
Dempster, John Benton
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t1959_Dempster.pdf
Adobe PDF, 11.18 MB
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1959-05
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Abstract
It is the purpose of this paper to compare the airplane frequency response functions of wing structural loads and airplane vertical accelerations due to random vertical gusts as determined theoretically by existing methods to those obtained experimentally. A measure of the accuracy for either method of determining the frequency- response functions may be gained through these comparisons.
Table of Contents
Preface -- Nomenclature -- List of tables and figures -- Introduction -- General considerations in the application of generalized harmonic analysis to gust loads on airplanes -- Experimental analysis -- Theoretical analysis -- Comparison of theoretical and experimental frequency-response functions -- Summary -- References
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Thesis (M.S.)-- University of Wichita, College of Engineering, Dept. of Aeronautical Engineering
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Wichita State University
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Wichita State University