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An investigation of the downwash at the probable tail location behind a high-aspect-ratio wing in the Langley 8-foot high-speed tunnel

机译：对兰利8英尺高速隧道中高纵横比机翼后方可能尾部位置下洗的调查

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作者
Whitcomb, Richard T;
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年度 1947
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Influence of Separated Wing Flow on Tail Downwash of Low-Wing Pusher Configuration [J] . K. Karthik, E. G. Tulapurkara, K. A. Damodaran Journal of Aircraft . 1999,第5期

机译：分离式机翼流对低翼推进器配置的尾部向下冲洗的影响
2. Wing-Body and Vertical Tail Interference Effects on Downwash Rate of the Horizontal Tail in Subsonic Flow [J] . Paziresh Ali, Nikseresht Amir Hossein, Moradi Hashem Journal of aerospace engineering . 2017,第4期

机译：亚音速流中机翼和垂直尾翼干扰对水平尾翼下冲率的影响
3. Investigation of wind tunnel wall effect and wing-fuselage interference regarding the prediction of wing aerodynamics and its influence on the horizontal tail [J] . Hoang Ngoc T. B., Bui Binh V. Journal of Mechanical Science and Technology . 2019,第6期

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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

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5. Wind tunnel, field and numerical investigations of plume downwash and dispersion at an arctic industrial site. [D] . Guenther, Alex Brian. 1989

机译：北极工业现场的风洞，羽流向下冲洗和扩散的现场和数值研究。
6. Test Capabilities and Recent Experiences in the NASA Langley 8-Foot High Temperature Tunnel [O] . Harvin Stephen F., Hodge Jeffrey S. 2000

机译：NASA Langley 8脚高温隧道的测试能力和最新经验

An investigation of the downwash at the probable tail location behind a high-aspect-ratio wing in the Langley 8-foot high-speed tunnel

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