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Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

机译：在超音速下具有任意扫掠和锥度的薄翼卷的理论升力和阻尼：超音速前缘和后缘

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作者
Harmon, Sidney M; Jeffreys, Isabella;
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年度 1950
页码 1-50
总页数 50
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WINGS, THIN - STABILITY; LIFT - WINGS, THIN; PRESSURE DISTRIBUTION - WINGS; THEORIES - FLOW - LINEAR; DAMPING IN ROLL; WINGS, SWEPTBACK - TAPERED; AIR FLOW - AIRFOILS - REVERSED; WINGS, SWEPTFORWRAD; ROLLING MOMENTS - WINGS, THIN; THEORIES - WINGS - SUPERSONIC;

机译：WINGs，THIN - sTaBILITY;提升 - 翅膀，薄;压力分布 - 翅膀;理论 - 流动 - 线性;滚动阻尼; WINGs，sWEpTBaCK - TapERED;空气流动 - 飞机 - 反转; WINGs，sWEpTFORWRaD;滚动的时刻 - 翅膀，薄;理论 - WINGs - sUpERsONIC;

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专利

1. Numerical research on the trailing-edge sweep of supersonic/transonic turbines [J] . Li Xin, Ji Lucheng, Zhou Ling Aerospace science and technology . 2020,第Apra期

机译：超音速/跨音速涡轮机后缘扫掠的数值研究
2. Flow behind castellated blunt-trailing-edge aerofoils at supersonic speeds [J] . Magi EC., Gai SL. Journal of Fluid Mechanics . 1998,第0期

机译：以超音速在带齿的钝尾缘翼型后方流动
3. TYPES OF FLOW OVER LEESIDE OF A SLENDER TAPERED WING AT SUPERSONIC SPEED [J] . 中国航空学报：英文版 . 1996,第003期

机译：超声速度下纤细锥形翼的LEESIDE的流动类型
4. Supersonic Flow Over Straight Shallow Cavities Including Leading and Trailing Edge Modifications [C] . S. Moon, S. Gai, H. Kleine, AIAA Fluid Dynamics Conference and Exhibit;AIAA/ASME Joint Thermophysics and Heat Transfer Conference;AIAA CFD High-Lift Prediction Workshop;HILIFTPW-1;AIAA Aerodynamic Measurement Technology and Ground Testing Conference;AIAA Applied Aerodynamics Conference;Plasmadynamics and Lasers Conference;Flow Control Conference . 2010

机译：超音速流在直的浅腔上的流动，包括前缘和后缘的修改
5. Static and dynamic analysis of a typical wing section with leading edge-trailing edge control surface configuration. [D] . Platanitis, George. 2003

机译：具有前缘-后缘边缘控制面配置的典型机翼部分的静态和动态分析。
6. Leading-edge vortices over swept-back wings with varying sweep geometries [O] . William B. Lambert, Mathew J. Stanek, Roi Gurka, 2019

机译：后掠翼上的前缘涡旋具有不同的掠掠几何形状
7. Estimation of Take-Off Performance for Supersonic Transport with Leading-Edge Vortex Flaps and Trailing-Edge Flaps [O] . Katsuhiro Miyata, Kenichi Rinoie 2003

机译：用前缘涡流襟翼和后缘襟翼估算超音速运输的起飞性能

Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

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