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Comparisons of methods of computing bending moments in helicopter rotor blades in the plane of flapping

机译：扑翼平面直升机旋翼叶片弯矩计算方法的比较

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作者
Luecker, Arthur R;
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年度 1945
页码 1-24
总页数 24
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ROTOR BLADES - BENDING MOMENTS; PROPELLERS, HELICOPTER; ROTOR BLADES - FLAPPING; FORMULAS - ROTORS - CIERVA;

机译：转子叶片 - 弯曲的时刻;螺旋桨，直升机;转子叶片 - FLappING;公式 - 转子 - CIERVa;

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1. MATHEMATICAL MODEL AND NUMERICAL METHOD FOR FLAP-TORSIONAL FLUTTER ANALYSIS OF HELICOPTER MAIN ROTOR BLADE [J] . S. A. Mikhailov, E. I. Nikolayev, N. A. Shilova Russian Aeronautics . 2004,第4期

机译：直升机主旋翼桨叶颤振颤振分析的数学模型和数值方法
2. Modelling and analysis of coupled flap-lag-torsion vibration characteristics helicopter rotor blades [J] . Pardo Alejandro Castillo, Goulos Ioannis, Pachidis Vassilios Proceedings of the Institution of Mechanical Engineers . 2017,第g10期

机译：直升机襟翼-滞后-扭转耦合振动特性的建模与分析
3. Modeling Helicopter Rotor Blade Flapping Motion Considering Nonlinear Aerodynamics [J] . Jyoti Ranjan Majhi, Ranjan Ganguli Computer Modeling in Engineering & Sciences . 2008,第1a2期

机译：考虑非线性空气动力学的直升机旋翼桨叶拍打运动建模
4. CALCULATION STUDY OF HELICOPTER ELASTIC ROTOR BLADE DEFORMATION IN PLANES OF PULL, ROTATION AND TORSION BY METHOD OF FORTH INTEGRATION [C] . V.A. Ivchin, I.O. Averyanov European rotorcraft forum . 2012

机译：用积分法计算拉，转，扭平面直升机弹性转子叶片的变形。
5. Effect of pitch angle and rotor speed on bending-bending elastic coupling of the CH149 Cormorant helicopter tail rotor blades. [D] . Laliberte, Maryse. 2012

机译：俯仰角和旋翼速度对CH149 Cormorant直升机尾桨叶片弯曲弯曲弹性联轴器的影响。
6. Examination of Inertial Sensor-Based Estimation Methods of Lower Limb Joint Moments and Ground Reaction Force: Results for Squat and Sit-to-Stand Movements in the Sagittal Plane [O] . Jun Kodama, Takashi Watanabe 2016

机译：基于惯性传感器的下肢关节力矩和地面反作用力估算方法的检验：矢状面下蹲和坐直运动的结果
7. Optimizing tuning masses for helicopter rotor blade vibration reduction including computed airloads and comparison with test data [O] . Wilbur Matthew L., Pritchard Jocelyn I., Walsh Joanne L., 1992

机译：优化调整质量以减少直升机旋翼桨叶的振动，包括计算的空气载荷并与测试数据进行比较

Comparisons of methods of computing bending moments in helicopter rotor blades in the plane of flapping

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