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Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company

机译：在Chance Vought aircraft Company提交的100英寸和弦NaCa 23016实际施工机翼部分的高雷诺数下拖动测量值

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作者
Nuber, Robert J;
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年度 1944
页码 1-5
总页数 5
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WIND TUNNEL TESTS - NACA - PRESURE, LOW-TURBULENCE (7 1/2' X 3'); AIRFOILS - NACA 23016 - CHARACTERISTICS; REYNOLDS NUMEBR; WINGS - VOUGHT WIND TUNNEL TESTS (NACA - PRESSURE, LOW-TURBULENCE); DRAG - WINGS;

机译：风洞隧道测试 - NaCa - 沉浸，低湍流（7 1/2'X 3'）; aIRFOILs - NaCa 23016 - 特点; REYNOLDs NUmEBR; WINGs - VOUGHT WIND TUNNEL TEsTs（NaCa - 压力，低湍流）; DRaG - WINGs;

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外文文献

1. Mean flow and turbulence measurements in the near field of a fighter aircraft wing-tip vortex at high Reynolds number and transonic flow conditions [J] . Fenella de Souza, Ben H.K. Lee ESAIM: Proceedings . 1999,第127期

机译：在高雷诺数和跨音速流动条件下的战斗机机翼尖端涡旋近场中的平均流量和湍流测量
2. 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
3. Lift and Drag Behavior of a low Reynolds Wing Section Submitted to a nearby stream wise vortex [C] . U. Boldes, J. Delnero, J. Colman, AIAA Aerospace Sciences Meeting and Exhibit . 2008

机译：雷诺兹机翼低断面顺流向附近涡流的起升和阻力行为
4. Mean flow and turbulence measurements in the near field of a fighter aircraft wing-tip vortex at high Reynolds number and transonic flow conditions [O] . Fenella de Souza, Ben H.K. Lee 1999

机译：在高雷诺数和跨音速流动条件下打架近场近场的平均流动和湍流测量
5. Drag Measurements at High Reynolds Numbers of a 100-Inch-Chord NACA 23016 Practical Construction Wing Section Submitted by Chance Vought Aircraft Company [R] . Von Doenhoff, A. E., Nuber, R. J. 1944

机译：在由机会沃特飞机公司提交了100英寸的和弦NaCa 23016现实建构翼段的高雷诺数拖动测量

Drag measurements at high Reynolds numbers of a 100-inch-chord NACA 23016 practical construction wing section submitted by Chance Vought Aircraft Company

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