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Flight Investigation to Determine the Equivalent Parasite Drag Area and Required Power of a Single Rotor Helicopter

机译：飞行调查确定等效的寄生虫拖曳区域和单个转子直升机所需的功率

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Tatsuya MASUE;
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年度 1965
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1. Investigation of Rotor Noise Shielding Effects by the Helicopter Fuselage in Forward Flight [J] . Yin Jianping Journal of Aircraft . 2019,第4期

机译：直升飞机机身对旋翼噪声的屏蔽作用研究
2. Investigations of synthetic jet control effects on helicopter rotor in forward flight based on the CFD method [J] . Zhao Q. -J., Chen X., Ma Y. -Yang, The Aeronautical Journal . 2018,第1253期

机译：基于CFD方法的合成射流控制对直升飞机旋翼的影响
3. Modelling the aeroelastic response and flight dynamics of a hingeless rotor helicopter including the effects of rotor-fuselage aerodynamic interaction [J] . Goulos I. The Aeronautical Journal . 2015,第1214期

机译：模拟无铰链旋翼直升机的气动弹性响应和飞行动力学，包括旋翼-机身气动相互作用的影响
4. Investigation of Rotor- Rotor Interactions for Two Helicopters in Forward Flight Using Free- Vortex Wake Methodology [C] . O. Yemenici, N. Sezer, O. Uzol AIAA Fluid Dynamics Conference and Exhibit;AIAA/ASME Joint Thermophysics and Heat Transfer Conference;AIAA CFD High-Lift Prediction Workshop;HILIFTPW-1;AIAA Aerodynamic Measurement Technology and Ground Testing Conference;AIAA Applied Aerodynamics Conference;Plasmadynamics and Lasers Conference;Flow Control Conference . 2010

机译：使用自由涡旋唤醒方法研究两架直升机在向前飞行中的转子-转子相互作用
5. Development of a simplified inflow model for a helicopter rotor in descent flight. [D] . Chen, Chang. 2006

机译：为下降中的直升机旋翼简化了进气模型的开发。
6. Mechanical power curve measured in the wake of pied flycatchers indicates modulation of parasite power across flight speeds [O] . L. Christoffer Johansson, Masateru Maeda, Per Henningsson, 2018

机译：捕蝇器唤醒后测得的机械功率曲线表明了跨飞行速度的寄生功率调制
7. Part I: A second approximation to the induced drag of a helicopter rotor in forward flight. Part II: The instantaneous induced velocity at the blade of a finite-bladed rotor in forward flight [O] . Prouty Raymond W. 1958

机译：第一部分：直升机旋翼在向前飞行中诱导阻力的第二个近似值。第二部分：前飞中有限叶片转子叶片的瞬时诱导速度
8. Simplified Aircraft Performance Methods: Power Required for Single and Tandem Rotor Helicopters in Hover and Forward Flight. [R] . Dietz, C. R. 1973

机译：简化的飞机性能方法：单悬架和串联转子直升机在悬停和前飞时所需的动力。

Flight Investigation to Determine the Equivalent Parasite Drag Area and Required Power of a Single Rotor Helicopter

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