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Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

机译：雷诺数为3.0 x 10（exp 6）和6.0 x 10（exp 6）的三个翼型截面的空气动力学特性是通过从NaCa 0012翼型截面的后部切下不同的量而形成的

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作者
Smith, Hamilton A; Schaefer, Raymond F;
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年度 1950
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS - NACA 0012 - CHAR , A C , MOMENTS & ORDINATES - HELICOPTER; AIRFOILS - CHARACTERISTICS - EFFECT OF SURFACE ROUGHNESS; AIRFOILS - CHARACTERISTICS - EFFECT OF RIVET HEADS; AIRFOILS - CHARACTERISTICS -EFFECT OF TRAILING-EDGE SHAPE; WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE;

机译：aIRFOILs - NaCa 0012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - 直升机;翼型 - 特性 - 表面粗糙度的影响;翼型 - 特征 - 铆头的影响;翼型 - 特征 - 拖尾形状的影响;风洞测试 - NaCa - 压力，低湍流;

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1. Turbulence modelling of the flow past a pitching NACA0012 airfoil at 10{sup}5 and 10{sup}6 Reynolds numbers [J] . G. Martinat, M. Braza, Y. Hoarau, Journal of Fluids and Structures . 2008,第8期

机译：雷诺数为10 {sup} 5和10 {sup} 6时经过俯仰NACA0012机翼的流动的湍流建模
2. Comparison of the Aerodynamic Characteristics of the NACA0012 Airfoil at Low-to-Moderate Reynolds Numbers for any Aspect Ratio [J] . S. Martínez-Aranda, A. L. García-González, L. Parras, International Journal of Aerospace Sciences . 2016,第1期

机译：在任何纵横比下，中低雷诺数下NACA0012机翼的空气动力学特性比较
3. Low-Reynolds-number effect on the aerodynamic characteristics of a pitching NACA0012 airfoil [J] . Dong-Ha Kim, Jo-Won Chang Aerospace science and technology . 2014,第1期

机译：低雷诺数对俯仰NACA0012翼型气动特性的影响
4. COMPARISON OF TWO ACTIVE FLOW CONTROL MECHANISMS OF PURE BLOWING AND PURE SUCTION ON A PITCHING NACA0012 AIRFOIL AT REYNOLDS NUMBER OF 1 × 10~6 [C] . EHSAN ASGARI, MEHRAN TADJFAR ASME Fluids Engineering Division Meeting . 2018

机译：在雷诺数1×10〜6的雷诺数纯吹制和纯吸液中的两个主动流量控制机制的比较1×10〜6
5. Study of 3-D Dynamic Roughness Effects on Flow Over a NACA 0012 Airfoil Using Large Eddy Simulations at Low Reynolds Numbers. [D] . Guda, Venkata Subba Sai Satish. 2015

机译：使用低雷诺数下的大型涡流模拟研究3-D动态粗糙度对流经NACA 0012翼型的影响。
6. Characteristics of the flow over a NACA 0012 airfoil at low Reynolds numbers [O] . R. W. Derksen, M. Agelinchaab, M. Tachie 2014

机译：在低雷诺数下NaCa 0012翼型上的流动特征
7. Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(6) and 6.0 x 10(6) of Three Airfoil Sections Formed by Cutting Off Various Amounts From the Rear Portion of the NACA 0012 Airfoil Section [R] . Smith, H. A., Schaefer, R. F. 1950

机译：在通过切断各种量从NaCa 0012翼型截面的后部形成的三个翼面区段的3.0×10（6）和6.0×10（6）雷诺数气动特性

Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

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