Dynamic load measurements on helicopter rotor blades of Russian origin

机译：俄罗斯起源直升机转子叶片的动态负荷测量

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The flight load measurement was carried out as a part of the long term plan for life extension of MI-8/MI-17 helicopters. The data will be used for fatigue testing of the tail rotor blade. Based on the experience, a methodology has been evolved to measure the loads in any typical loading environment for the helicopter components. The work was carried out as a team involving members from design, operations, research and certification agencies.

机译：飞行负荷测量是作为MI-8 / MI-17直升机寿命延伸的长期计划的一部分。数据将用于尾转子叶片的疲劳测试。基于这种经验，已经演化了方法，以测量直升机组分的任何典型装载环境中的负载。这项工作是作为涉及设计，运营，研究和认证机构的成员的团队进行的。

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《National seminar on aerospace structures》|2002年||共6页
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K. Venkatarman; R. Arunagiri; Balakrishna; K. K. Brahma;
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中图分类 V14;
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1. Effects of blade configuration parameters on helicopter rotor structural dynamics and whirl tower loads [J] . Kumar M. Rohin, Venkatesan C. The Aeronautical Journal . 2016,第1224期

机译：叶片配置参数对直升机旋翼结构动力学和旋风塔载荷的影响
2. Multidisciplinary Aerodynamic Design of a Rotor Blade for an Optimum Rotor Speed Helicopter [J] . Jiayi Xie, Zhifeng Xie, Ming Zhou, Applied Sciences . 2017,第6期

机译：最优旋翼直升机旋翼的多学科空气动力学设计
3. Multidisciplinary Aerodynamic Design of a Rotor Blade for an Optimum Rotor Speed Helicopter [J] . Jiayi Xie, Zhifeng Xie, Ming Zhou, Applied Sciences . 2017,第6期

机译：最优旋翼直升机旋翼的多学科空气动力学设计
4. Dynamic load measurements on helicopter rotor blades of Russian origin [C] . K. Venkatarman, R. Arunagiri, Balakrishna, National seminar on aerospace structures . 2002

机译：俄罗斯起源直升机转子叶片的动态负荷测量
5. DYNAMICS OF A HELICOPTER WITH A SLING LOAD (ROTOR DOWNWASH, MILVAN, UNSTEADY AERODYNAMICS, CH-53, TRIM). [D] . RONEN, TUVYA. 1986

机译：带有吊索载荷的直升机的动力学特性（转子下降，米尔文，不稳定气动，CH-53，TRIM）。
6. Noise Cancellation of Helicopter Blade Deformations Measurement by Fiber Bragg Gratings [O] . Raoul R. Nigmatullin, Timur Agliullin, Sergey Mikhailov, 2021

机译：纤维布拉格光栅测量直升机叶片变形的噪声消除
7. A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter. [O] . Balcerak, John C. 1967

机译：一种预测串联旋翼直升机转子叶片的气动载荷和动态响应的方法。
8. In-Flight Measurement of Rotor Blade Airloads, Bending Moments, and Motions, Together with Rotor Shaft Loads and Fuselage Vibration, on a Tandem Rotor Helicopter. Volume V. Investigation of Blade Stall Conditions [R] . Pruyn, R. R. 1968

机译：在串联转子直升机上飞行测量转子叶片空气负载，弯曲力矩和运动，以及转子轴负载和机身振动。第五卷叶片失速条件的研究

Dynamic load measurements on helicopter rotor blades of Russian origin

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