Vibration Reduction in Rotorcraft using Actively Controlled Flap - from Theoretical Concept to Flight Ready Hardware
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- SKU # : sm_aeromech_2004_0031
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Vibration Reduction in Rotorcraft using Actively Controlled Flap - from Theoretical Concept to Flight Ready Hardware
Authors / Details: P. Friedmann, Univ. of MichiganRecently Viewed Items
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