A limited flight investigation of the effect of dynamic vibration absorbers on the response of an airplane structure during buffeting
Description:
Report presenting limited flight measurements made in order to investigate the effect of dynamic vibration absorbers on the structural response of a Lockheed F-80A airplane during buffeting. The results were obtained by comparison of data with and without the absorbers operating through use of electrical frequency-analysis techniques.
Date:
January 25, 1955
Creator:
Thompson, Jim Rogers & Yeates, John E., Jr.
Item Type:
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Partner:
UNT Libraries Government Documents Department