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Flight tests of the Sikorsky HNS-1 (Army YR-4B) helicopter II : hovering and vertical-flight performance with the original and an alternate set of main-rotor blades, including a comparison with hovering performance theory

机译：西科斯基HNs-1（陆军YR-4B）直升机II的飞行试验：使用原始和另一组主转子叶片的悬停和垂直飞行性能，包括与悬停性能理论的比较

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作者
Gessow, Alfred;
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年度 1945
页码 1-15
总页数 15
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ROTOR BLADES; PROPELLERS, HELICOPTER; HELICOPTERS-SIKORSKY HNS-1 FLIGHT TESTS (AMER );

机译：转子叶片;螺旋桨，直升机;直升机-sIKORsKY HNs-1飞行测试（美国）;

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1. Aerodynamic design optimization of helicopter rotor blades including airfoil shape for hover performance [J] . Ngoc Anh Vu, Jae Woo Lee, Jung Il Shu 中国航空学报（英文版） . 2013,第001期

机译：直升机旋翼桨叶的气动设计优化，包括翼型形状，以实现悬停性能
2. Navier-Stokes Prediction of Helicopter Rotor Performance in Hover Including Aeroelastic Effects [J] . P. Beaumier, E. Chelli, K. Pahlke Journal of the American Helicopter Society . 2001,第4期

机译：悬停时包括气动弹性效应的直升机旋翼性能的Navier-Stokes预测
3. Iterative Blade Element Momentum Theory for Predicting Coaxial Rotor Performance in Hover [J] . Seongkyu Lee, Maxime Dassonville Journal of the American Helicopter Society . 2020,第4期

机译：迭代叶片元件动量理论，用于预测悬停中同轴转子性能
4. Navier-stokes prediction of helicopter rotor performance in hover including aero-elastic effects [C] . P.Beaumier, E.Chelli, K.Pahlke AHS international annual forum . 2000

机译：Navier-stokes预测直升机旋翼在悬停中的性能，包括气动弹性效应
5. Study of counter-rotating coaxial rotors in hover: A performance model based on blade element theory including swirl velocity. [D] . Lucas, Florent. 2007

机译：悬停中同轴旋转同轴转子的研究：一种基于叶片元素理论的性能模型，包括涡旋速度。
6. Aerodynamic design optimization of helicopter rotor blades including airfoil shape for hover performance [O] . Vu Ngoc Anh, Lee Jae Woo, Shu Jung Il 2013

机译：直升机旋翼桨叶的气动设计优化，包括翼型形状，以实现悬停性能

Flight tests of the Sikorsky HNS-1 (Army YR-4B) helicopter II : hovering and vertical-flight performance with the original and an alternate set of main-rotor blades, including a comparison with hovering performance theory

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