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Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hovering

机译：侧翼倾转翼VTOL模型研究确定悬停时偏航控制全跨度襟翼的地面效应

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Hovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control

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作者
Grunwald, K. J.;
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年度 1966
页码 1-75
总页数 75
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FLAPPING; GROUND EFFECT (AERODYNAMICS); HOVERING; SEMISPAN MODELS; TILT WING AIRCRAFT; VERTICAL TAKEOFF AIRCRAFT; YAW; GROUND EFFECT; HOVERING; SEMISPAN MODEL; TILT-WING AIRCRAFT; VTOL AIRCRAFT;

机译：扑;地面效应（空气动力学）;徘徊; sEmIspaN模型; TILT WING aIRCRaFT;垂直起飞飞机;偏航;地面效应;徘徊; sEmIspaN模型; TILT-WING aIRCRaFT; VTOL aIRCRaFT;

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专利

1. Accurate Modeling and Robust Hovering Control for a Quad–rotor VTOL Aircraft [J] . Jinhyun Kim, Min-Sung Kang, Sangdeok Park Journal of Intelligent & Robotic Systems . 2010,第1a4期

机译：四旋翼垂直起降飞机的精确建模和鲁棒悬停控制
2. Accurate Modeling and Robust Hovering Control for a Quad-rotor VTOL Aircraft [J] . Jinhyun Kim, Min-Sung Kang, Sangdeok Park Journal of Intelligent & Robotic Systems: Theory & Application . 2010,第1a4期

机译：四旋翼垂直起降飞机的精确建模和鲁棒悬停控制
3. Investigation of full and partial ground effects on a flapping foil hovering above a finite-sized platform [J] . Wang Lu, Yeung Ronald W. Physics of fluids . 2016,第7期

机译：悬停在有限尺寸平台上方的拍打箔上的全部和部分地面效应的研究
4. NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development [C] . Paul M. Rothhaar, Patrick C. Murphy, Barton J. Bacon, AIAA aviation technology, integration and operations conference;AIAA aviation forum . 2014

机译：NASA Langley分布式推进VTOL倾斜翼飞机测试，建模，模拟，控制和飞行测试开发
5. Flapping flight for biomimetic robotic insects: System modeling and flight control in hover. [D] . Deng, Xinyan. 2004

机译：仿生机器人昆虫的扑翼飞行：悬停中的系统建模和飞行控制。
6. Development of Model Predictive Controller for a Tail-Sitter VTOL UAV in Hover Flight [O] . Boyang Li, Weifeng Zhou, Jingxuan Sun, 2018

机译：悬停飞行尾座垂直起降无人机的模型预测控制器的开发
7. A qualitative discussion of the stability and control of VTOL aircraft during hover (out of ground effect) and transition. [O] . Weitz Paul J. 1964

机译：对VTOL飞机在悬停（脱离地面影响）和过渡期间的稳定性和控制进行定性讨论。
8. Investigation of a Semispan Tilt-Wing VTOL Model to Determine Ground Effect on Full-Span Flaps Used for Yaw Control in Hovering [R] . Grunwald, K. J. 1966

机译：半桅倾斜翼垂直起降模型确定悬停偏航控制全跨翼襟翼地面效应的研究

Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hovering

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