首页> 美国政府科技报告 >Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios

【24h】

Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios

机译：在翼型截面的NaCa二维低湍流隧道中进行测试，设计具有小俯仰力矩和高升阻比

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Tetervin, Neal;
展开▼
作者单位

展开▼
年度 1943
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOIL SURFACES-ROUGHNESS; AIRFOILS-NACA 23015-CHAR , A C , MOMENTS & ORDINATES; MACH NUMBER; REYNOLDS NUMBER; LIFT & DRAG RATIO; WINGS, ROTATING; DRAG, PROFILE; PITCHING MOMENTS-AIRFOILS-NACA; AIRFOILS-ROTOR BLADES; PRESSURE DISTRIBUTION-AIRFOILS-NACA HELICOPTER;

机译：翼型表面 - 粗糙度; aIRFOILs-NaCa 23015-CHaR，a C，mOmENTs＆amp;坐标;马赫数; REYNOLDs NUmBER; LIFT＆amp; DRaG RaTIO; WINGs，ROTaTING; DRaG，pROFILE; pITCHING mOmENTs-aIRFOILs-NaCa; aIRFOILs-ROTOR BLaDEs;压力分布 - 机翼 - NaCa直升机;

相似文献

外文文献
中文文献
专利

1. OPTIMIZATION OF THE SLOT SUCTION OF AIR FROM A CIRCULAR VORTEX CELL ON A THICK NACA0022 AIRFOIL WITH A MAXIMUM LIFT-DRAG RATIO [J] . S. A. Isaev, E. I. Kalinin, A. G. Sudakov, Journal of engineering physics and thermophysics . 2015,第6期

机译：优化具有最大升降比的厚NACA0022机翼上圆形涡流细胞的吸入空气
2. Two-dimensional Low-reynolds Number Wind Tunnel Results For Airfoil Naca 0018 [J] . W.A. Timmer Wind Engineering . 2008,第6期

机译：翼型Naca 0018的二维低雷诺数风洞结果
3. Two-dimensional Low-reynolds Number Wind Tunnel Results For Airfoil Naca 0018 [J] . W.A. Timmer Wind Engineering . 2008,第6期

机译：翼型Naca 0018的二维低雷诺数风洞结果
4. Aerodynamic Moment Analysis of an Aeroelastic NACA 0012 Airfoil Oscillating in Pitch at Transitional Reynolds Numbers [C] . Y. Harris, D. Poirel 21st Canadian Congress of Applied Mechanics(CANCAM 2007) . 2007

机译：空气弹性NACA 0012翼型在过渡雷诺数下在桨距中振荡的气动力矩分析。
5. Localisation of flow separation and transition over a pitching NACA0012 airfoil at transitional Reynolds number. [D] . Rudmin, Daniel. 2013

机译：流分离和过渡在过渡雷诺数的俯仰NACA0012机翼上的定位。
6. Generation of the pitch moment during the controlled flight after takeoff of fruitflies [O] . Mao Wei Chen, Jiang Hao Wu, Mao Sun 2012

机译：果蝇起飞后受控飞行期间俯仰力矩的产生
7. Wind tunnel tests of the NACA 63-415 and a modified NACA 63-415 airfoil [O] . Bak C., Fuglsang P., Johansen J., 2000

机译：NaCa 63-415和改进的NaCa 63-415翼型的风洞试验
8. TESTS IN THE NACA TWO-DIMENSIONAL LOW-TURBULENCE TUNNEL OF AIRFOIL SECTIONS DESIGNED TO HAVE SMALL PITCHING MOMENTS AND HIGH LIFT-DRAG RATIOS [R] . Neal Tetervin 1943

机译：在NaCa二维低湍流隧道中的测试设计为具有小倾斜距离和高升降比的翼型截面

Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios

摘要

著录项

相似文献

相关主题

期刊订阅