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CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume V. Plotted Aft Rotor Blade Chord Torsion and Absolute Loads

机译：CH-46复合材料转子叶片飞行应力测量数据。第五卷。绘制后转子叶片弦扭转和绝对载荷

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摘要

This volume contains measured steady and alternating aft rotor blade chord, torsion and absolute loads plotted versus true airspeed. The same data is tabulated in Volume 10.

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作者
Aiello, R.; Bendo, J.;
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年度 1978
页码 p.1-326
总页数 326
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; Tensile stress; Torsion; Airspeed; Flight testing; Flight maneuvers; Aerodynamic loading; Data bases; Graphs; Helicopters;

机译：转子叶片（旋翼）;复合材料;飞行载荷;直升机转子;应力;弯曲应力;拉伸应力;扭转;空速;飞行试验;飞行机动;空气动力学载荷;数据库;图形;直升机;

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专利

1. SIMULTANEOUS SOLUTION OF A PROBLEM ON LOADING THE MAIN ROTOR BLADE AND TORSION BARS IN HELICOPTER FLIGHT [J] . A. Yu. Liss Russian Aeronautics . 2003,第4期

机译：同时解决直升机飞行中主旋翼和扭杆加载的问题
2. Simultaneous Solution of a Problem on Loading the Main Rotor Blade and Torsion Bars in Helicopter Flight [J] . A. YU. LISS Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第4期

机译：直升机飞行中主旋翼和扭杆加载问题的同时解决
3. Simultaneous Solution of a Problem on Loading the Main Rotor Blade and Torsion Bars in Helicopter Flight [J] . A. YU. LISS Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第4期

机译：同时解决装载主转子叶片和直升机飞行的扭杆的问题
4. K-MAX ROTOR BLADE FLIGHT LOADS SURVEY FOR OUT OF ENVELOPE FLIGHT TEST [C] . Fu-Shang (John) Wei, Frank Gallagher AHS International annual forum . 2008

机译：超出飞行测试的K-MAX旋翼桨叶飞行载荷调查
5. DYNAMIC STABILITY OF HINGELESS AND BEARINGLESS ROTOR BLADES IN FORWARD FLIGHT (ROTORCRAFT, FINITE ELEMENT). [D] . PANDA, BRAHMANANDA. 1985

机译：前向飞行中无铰链和无轴承转子叶片的动态稳定性（旋翼飞机，有限元）。
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 V. Plotted Aft Rotor Blade Chord Torsion and Absolute Loads

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