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CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume II. Plotted Forward Rotor Blade Angles and Flap Loads

机译：CH-46复合材料转子叶片飞行应力测量数据。第二卷。绘制前转子叶片角度和襟翼载荷

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This volume contains measured steady and alternating forward rotor blade angles and flap loads plotted versus true airspeed. The same data is tabulated in Volume 9.

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作者
Aiello, R.; Bendo, J.;
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年度 1978
页码 p.1-319
总页数 319
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Rotor blades(Rotary wings); Composite materials; Flight loads; Helicopter rotors; Stresses; Bending stress; Flight testing; Flight maneuvers; Aerodynamic loading; Pitch(Inclination); Airspeed; Data bases; Graphs; Helicopters;

机译：转子叶片（旋转翼）;复合材料;飞行载荷;直升机转子;应力;弯曲应力;飞行试验;飞行机动;空气动力载荷;俯仰（倾斜）;空速;数据库;图形;直升机;

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专利

1. Aeroelastic Stability Analysis of Composite Helicopter Rotor Blades in Hover and Forward Flight [J] . In Lee, Min-Soo Jeong, Seung-Jae Yoo 复合材料シンポシウム讲演要旨集． . 2013,第38期

机译：复合直升机旋翼盘旋和向前飞行的气动弹性稳定性分析。
2. Aeroelastic response and stability analysis of composite rotor blades in forward flight [J] . S.M. Jeon, I. Lee Composites. B . 2001,第3期

机译：复合材料转子叶片前向飞行的气动弹性响应和稳定性分析
3. Blade runners: Van Horn Aviation fast-tracks in-house testing to prove its composite helicopter rotor blades beat legacy metal rotors [J] . FRANK COLUCCI Aerospace Testing International . 2015,第Sepa期

机译：叶片赛跑者：Van Horn Aviation快速通道进行了内部测试，证明其复合直升机旋翼桨叶击败了传统金属旋翼
4. AEROELASTIC STABILITY, RESPONSE AND LOADS OF SWEPT TIP COMPOSITE ROTOR BLADES IN FORWARD FLIGHT [C] . Kuo-An Yuan, Peretz P. Friedmann, Comandur Venkatesan AIAA/ASME/ASCE/AHS/ASC, structures, structural dynamics, and materials conference . 1994

机译：飞行中扫除尖端复合转子叶片的空气弹性稳定性，响应和载荷
5. ROTOR BLADE FLAP-LAG STABILITY AND RESPONSE IN FORWARD FLIGHT IN TURBULENT FLOWS. [D] . SHIAU, TING-NUNG BERNARD. 1984

机译：湍流中转子叶片的襟翼滞后稳定性和正向飞行响应。
6. Process Modeling of Composite Materials for Wind-Turbine Rotor Blades: Experiments and Numerical Modeling [O] . Birgit Wieland, Sven Ropte 2017

机译：风力涡轮机转子叶片复合材料的过程建模：实验和数值建模
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

CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume II. Plotted Forward Rotor Blade Angles and Flap Loads

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