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Investigation of a spoiler-type lateral control system on a wing with full-span flaps in the Langley 19-foot pressure tunnel

机译：在Langley 19英尺压力隧道中对具有全跨度襟翼的机翼上的扰流式横向控制系统的研究

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作者
Deters, Owen J; Russell, Robert T;
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年度 1947
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WING SPOILERS & AILERONS; WING FLAPS, SLOTTED - DOUBLE; WING FLAPS, SLOTTED - DOUBLE; WING FLAPS - DEFLECTION; WIND TUNNEL TESTS - NACA - PRESSURE (19') WORK CARRIED ON LMAL; WING SPOILERS - HINGE MOMENTS; LATERAL CONTROL DEVICES WORK CARRIED ON AT LMAL; WING FLAPS, SLOTTED & AILERONS; AIRPLANES, BOMBING;

机译：WING spOILERs＆amp;副翼;翅膀，开口 - 双倍;翅膀，开口 - 双倍;翼片 - 挠曲;风洞测试 - NaCa - 压力（19'）工作在LmaL; WING spOILERs - HINGE mOmENTs;侧面控制装置在LmaL上工作; WING FLaps，sLOTTED＆amp;副翼;飞机，炸弹;

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1. Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps [J] . Kanistras Konstantinos, Saka Pranith Chander, Valavanis Kimon P., Journal of Aircraft . 2018,第4期

机译：双半径襟翼循环控制机翼的风洞研究
2. Effect of Full-Span Gurney Flap Height on Wing Wake Vortex Alleviation [J] . Vojin R. Nikolic Journal of Aircraft . 2006,第5期

机译：全跨格尼襟翼襟翼高度对机翼尾流涡流缓解的影响
3. Full-Span Flying Wing Wind Tunnel Test: A Body Freedom Flutter Study [J] . Pengtao Shi, Jihai Liu, Yingsong Gu, Fluids . 2020,第1期

机译：全跨飞翼风隧道试验：一项翼翼的浮动研究
4. An Experimental Investigation of a Wing-Fuselage Junction Model in the NASA Langley 14- by 22-Foot Subsonic Wind Tunnel [C] . Michael A. Kegerise, Dan H. Neuhart, Judith A. Hannon, AIAA SciTech forum and exposition . 2019

机译：NASA兰利14英尺乘22英尺亚音速风洞的机翼-机身交界处模型的实验研究
5. Wind tunnel test of a tailless aircraft with a belly-flap control surface used in combination with wing flaps. [D] . Dougherty, Daniel A. 2012

机译：带有襟翼控制面并与机翼襟翼配合使用的无尾飞机的风洞测试。
6. Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design Numerical Simulation and Wind Tunnel Experimental Testing [O] . Shehryar Khan, Teodor Lucian Grigorie, Ruxandra Mihaela Botez, 2019

机译：变形翼尖驱动系统的基于模糊逻辑的控制：设计数值模拟和风洞实验测试
7. Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50 [O] . Babister A. W. 1951

机译：具有后缘分裂式襟翼的后掠翼的压力分布测量：航空学院风洞工作总结1948-50

Investigation of a spoiler-type lateral control system on a wing with full-span flaps in the Langley 19-foot pressure tunnel

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