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Performance and Airloads Analyses for a Rigid Coaxial Rotor of High-Speed Compound Unmanned Rotorcrafts
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J. KIMS Technol. 2020;23(4):311-318. Published online 2020 Aug 5 DOI: https://doi.org/10.9766/KIMST.2020.23.4.311
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Citations to this article as recorded by
 Airframe Vibration Reduction for an Unmanned Lift-Offset Compound Helicopter Using Active Vibration Control System
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