Effect of Piezoelectric Hysterisis Nonlinearity on Helicopter Vibration Control Using Trailing Edge Flaps
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
2005-01-01
Conference paper
Electronic Resource
English
Effect of Piezoelectric Hysteresis on Helicopter Vibration Control Using Trailing-Edge Flaps
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|Helicopter vibration reduction with trailing edge flaps
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|Helicopter Vibration Reduction with Trailing Edge Flaps
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|Helicopter Vibration Reduction with Trailing Edge Flaps
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