Flexible airplane structures in presence of excitation forces may oscillate with bounded or unbounded motion; vehicle safety and durability depend on control and reduction of vibration; designers can generally safeguard against its occurrence by tuning airframe; supplementing design function are experimental studies that identify dynamic response characteristics for aeroelastic and fatigue considerations; experimental methodology, based on fundamental engineering principles and basic laboratory instrumentation, is described together with examples which demonstrate directness and efficiency obtainable.
Airplane vibration -- Practical approach
SAE -- Business Aircraft Conf -- Proc
Proceedings of SAE -- Business Aircraft Conference ; 1965 Vibrations
1965
9 pages
Conference paper
English
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