Sonic Fatigue Design Data for Bonded Aluminum Aircraft Structures
Description:
Report describing a combined analytic and experimental program conducted to determine the sonic fatigue design properties of bonded structural sections based on skin-stringer-frame design commonly applied in aircraft and to formulate data and criteria for the development of sonic fatigue resistant designs of such structure. Beam tests were conducted under narrow band shaker excitation and multibay panel tests were conducted under broadband acoustic excitation. The test results are evaluated for…
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Date:
June 1977
Creator:
Jacobson, Marcus J.
Partner:
UNT Libraries Government Documents Department