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Airfoil section data from tests of 10 practical- construction sections of helicopter rotor blades submitted by the Sikorsky Aircraft Division, United Aircraft Corporation

机译：联合飞机公司西科斯基飞机部提交的直升机旋翼桨叶的10个实际结构部分的测试中的翼型截面数据

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作者
Tetervon, Neal;
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年度 1944
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
HELICOPTERS - SIKORSKY R (EXPERIMENTAL) (AMER ); AIRFOILS, HELICOPTER; AIRFOILS - SIKORSKY - CHAR , A C & MOMENTS - HELICOPTER; WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE (7 1/2' X 3');

机译：直升机 - sIKORsKY R（实验）（美国）;飞机，直升机; aIRFOILs - sIKORsKY - CHaR，a C＆amp;时刻 - 直升机;风洞测试 - NaCa - 压力，低湍流（7 1/2'X 3'）;
入库时间 2022-08-29 11:20:30

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机译：西科斯基完成CH-53K直升机首批旋翼桨叶的初始测试
2. Experimental Techniques for Evaluation of Fatigue Characteristics of Laminated Constructions from Composite Materials:Full-Scale Testing of the Helicopter Rotor Blades [J] . Bosko Rasuo Journal of testing and evaluation . 2011,第2期

机译：用复合材料评估层合结构疲劳特性的实验技术：直升机旋翼桨叶的全面测试
3. New Solutions for Aircraft Wing and Helicopter Blade Airfoils [C] . Constantin Rotaru, Mihai Mihaila-Andres International Conference on Mathematics and Computers in Sciences and in Industry . 2016

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4. Performance and Vibratory Loads Data From a Wind-Tunnel Test of a Model Helicopter Main-Rotor Blade With a Paddle-Type Tip [O] . Singleton, Jeffrey D., Yeager, William T., Jr., Noonan, Kevin W., 1997

机译：性能和振动载荷数据来自带有桨式尖端的模型直升机主旋翼桨叶的风洞试验

Airfoil section data from tests of 10 practical- construction sections of helicopter rotor blades submitted by the Sikorsky Aircraft Division, United Aircraft Corporation

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