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Profile Drag Measurements on Hurricane II Z.3687 Fitted with Special Wings of 'Low Drag' Section built by Armstrong Whitworth Aircraft Ltd

机译：飓风II Z.3687合身形状阻力测量与阿姆斯壮Whitworth飞公司建立“低风阻”节特别翅膀

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作者
Plascott, R. H.;
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年度 1946
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Low drag ; Aircraft ; United kingdom ; Wings ; Measurement ; Profiles;

机译：低阻力;飞机;英国;翅膀;测量;型材;

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1. Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speeds, Part Ⅱ-Experimental validation using Infra-Red transition measurement from Wind Tunnel tests [J] . Andreea Koreanschi, Oliviu Sugar Gabor, Joran Acotto, 中国航空学报（英文版） . 2017,第001期

机译：用于低速降低阻力的飞机变形翼尖演示器的优化和设计，第二部分-使用风洞试验的红外过渡测量进行实验验证
2. Optimization and design of an aircraft's morphing wing-tip demonstrator for drag reduction at low speed, Part Ⅰ–Aerodynamic optimization using genetic, bee colony and gradient descent algorithms [J] . Andreea Koreanschi, Oliviu Sugar Gabor, Joran Acotto, 中国航空学报（英文版） . 2017,第001期

机译：用于低速降低阻力的飞机变形翼尖演示器的优化和设计，第一部分–使用遗传，蜂群和梯度下降算法进行空气动力学优化
3. Optimal Low-Drag Wing Planforms for Tractor-Configuration Propeller-Driven Aircraft [J] . Rakshith B. R., Deshpande S. M., Narasimha Roddam, Journal of Aircraft . 2015,第6期

机译：拖拉机配置螺旋桨驱动飞机的最佳低阻力机翼计划
4. Zero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Conceptual Design [C] . T. Takahashi, B. German, A. Shajanian, AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

机译：飞机概念设计中有限机翼的零升力阻力和阻力发散预测
5. CFD Investigation of the Drag Effects on an Aircraft by Means of Altering the Wing or Canard Size and Position [D] . Brown, Taylor. 2021

机译：通过改变机翼或迫鸭尺寸和位置，CFD对飞机上的阻力效应进行调查
6. Velocity profiles of oscillating arterial flow with some calculations of viscous drag and the Reynolds number [O] . J. F. Hale, D. A. McDonald, J. R. Womersley 1955

机译：振荡动脉血流的速度分布并计算了粘性阻力和雷诺数
7. Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II \u2013 Experimental validation using infra-red transition measurements during wind tunnel tests [O] . Koreanschi, Andreea, Gabor, Oliviu Sugar, Acotto, Joran, 2017

机译：优化和设计用于降低低速风阻的变形翼尖飞机演示器，第二部分\ u2013在风洞测试期间使用红外过渡测量进行实验验证

Profile Drag Measurements on Hurricane II Z.3687 Fitted with Special Wings of 'Low Drag' Section built by Armstrong Whitworth Aircraft Ltd

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