The rotor and the fuselage of the helicopter are mechanically coupled at the rotor hub. A coupled rotor/ fuselage vibration analysis is performed by the matching of rotor and fuselage impedance at the rotor hub.

  • 直升机的旋翼与机身在桨毂处是机械耦合的,用旋翼阻抗和机身阻抗在桨毂处匹配的方法分析旋翼/机身耦合系统的固有特性。

  • 互联网摘选 2025-03-01 14:20:36

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