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Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel

机译：沉水管道安装的上一个改良战斗机飞机在ames试验40- 80英尺风洞

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作者
Martin, N. J.;
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年度 1947
页码 p.1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aircraft engine ducts ; Installation ; Wind tunnel tests ; Underwater ; Fighter aircraft ; Ducts;

机译：飞机发动机管道;安装;风洞试验;水下;战斗机;线槽;

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1. Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel [J] . I-ChungChang, Thomas R.Norman, Ethan A.Romander International journal of aerospace engineering . 2014,第3期

机译：UH-60A转子在40 x 80英尺风洞内的空气负荷相关性
2. Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel [J] . I-Chung Chang, Thomas R. Norman, Ethan A. Romander International journal of aerospace engineering . 2014,第期

机译：UH-60A转子在40 x 80英尺风洞内的空气负荷相关性
3. Free-to-Roll Testing of Airplane Models in Wind Tunnels [J] . NASA Tech Briefs . 2007,第11期

机译：风洞中飞机模型的免费滚动测试
4. Acoustic Testing of the Tiltrotor Test Rig in the National Full-Scale Aerodynamics Complex 40- by 80-Foot Wind Tunnel [C] . Natasha L. Schatzman, Carlos Malpica Annual Vertical Flight Society forum and technology display . 2019

机译：国家全尺寸空气动力学综合体40 x 80英尺风洞中的倾转仪试验台的声学测试
5. Reconfigurable flight control for high angle of attack fighter aircraft, with wind tunnel study [D] . Siddiqui, Bilal Ahmed 2010

机译：高攻角战斗机的可重构飞行控制，带有风洞研究
6. A New Position Measurement System Using a Motion-Capture Camera for Wind Tunnel Tests [O] . Hyo Seon Park, Ji Young Kim, Jin Gi Kim, 2013

机译：使用运动捕捉相机进行风洞测试的新型位置测量系统
7. Airloads Correlation of the UH-60A Rotor Inside the 40- by 80-Foot Wind Tunnel [O] . Romander Ethan A., Norman Thomas R., Chang I-Chung 2013

机译：UH-60A转子在40 x 80英尺风洞内的空气载荷相关性

Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel

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