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Effect of Lift-offset Rotor Hub Vibratory Load Components on Airframe Vibration Responses of High-Speed Compound Unmanned Rotorcrafts
Ji-Su Kim, Sung-Boo Hong, Young-Min Kwon, Jae-Sang Park
J. KIMS Technol. 2021;24(3):255-263.   Published online June 5, 2021
DOI: https://doi.org/10.9766/KIMST.2021.24.3.255

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Effect of Lift-offset Rotor Hub Vibratory Load Components on Airframe Vibration Responses of High-Speed Compound Unmanned Rotorcrafts
Journal of the Korea Institute of Military Science and Technology. 2021;24(3):255-263   Crossref logo
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Performance and Airloads Analyses for a Rigid Coaxial Rotor of High-Speed Compound Unmanned Rotorcrafts
Journal of the Korea Institute of Military Science and Technology. 2020;23(4):311-318   Crossref logo
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Aerodynamically induced noise of a lift-offset coaxial rotor with pitch attitude in high-speed forward flight
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Journal of the Korea Institute of Military Science and Technology. 2021;24(4):357-367   Crossref logo
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Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System
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Variable rotor speed strategy for coaxial compound helicopters with lift–offset rotors
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A Method of Hub Vibratory Load Prediction under High Speed State
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A Compound Vibratory Mode in High Speed Vibratory Tapping
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Impulsive Loading Noise of a Lift-Offset Coaxial Rotor in High-Speed Forward Flight
AIAA Journal. 2020;58(2):687-701   Crossref logo
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