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The airframe transfer function in dynamic stability flight testing
Hagenau, Karl Heinz
Hagenau, Karl Heinz
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t1963_Hagenau.pdf
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1963-06
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Thesis
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Abstract
Considerable effort has been made by aeronautical research organizations and industry during the last decade to find suitable experimental flight test methods for the evaluation of the dynamic characteristics of an aircraft. The reference material which culminated from this effort was reviewed with the following objectives:
1. To determine the present state of the art of dynamic
stability flight testing from a literature survey.
2. To document selected methods in a form suitable
for introducing a flight test organization to the concepts
of dynamic stability testing.
3. To investigate applicability of these techniques
to the B-52 airplane.
The results of this study were formulated into this thesis.
Table of Contents
The history of dynamic stability flight testing -- Selected techniques in dynamic stability testing; Steady state sinusoidal response, transient response, the control system input, the airframe transient response, the airframe transfer function -- Application to the B-52 airplane -- Summary -- Bibliography
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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