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Measurements of aerodynamic characteristics of a 35 degree sweptback NACA 65-009 airfoil model with 1/4-chord bevelled-trailing-edge flap and trim tab by the NACA wing-flow method

机译：使用NaCa翼流法测量35度后掠NaCa 65-009翼型模型的空气动力学特性，该模型具有1/4弦斜切边缘襟翼和纵倾翼片

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Johnson, Harold I; Brown, B Porter;
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年度 1950
页码 1-71
总页数 71
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Ground effect on the aerodynamics of a naca 0015 airfoil with a plain trailing-edge flap [J] . V Tremblay Dionne, T Lee Fluid Mechanics Research International Journal . 2018,第1期

机译：地面对带有平尾缘襟翼的naca 0015机翼的空气动力学的影响
3. The effects of Gurney flap on the aerodynamic performance of NACA 0012 airfoil in the rarefied gas flow [J] . Amini Y., Liravi M., Izadpanah E. Computers & Fluids . 2018,第期

机译：Gurney PLAP对稀土气流NaCA 0012翼型空气动力学性能的影响
4. Numerical investigation of gurney flap aerodynamics over a NACA 2412 airfoil [C] . Sanjoy Kumar Saha, Mahbubul Alam, A. B. M. Toufique Hasan International Conference on Mechanical Engineering . 2018

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5. Direct Numerical Simulations of a Cambered NACA 65(1)-412 Airfoil at Low Reynolds Numbers: Flow Separation, Instabilities and Lagrangian Aerodynamics [D] . Klose, Bjoern Fabian. 2021

机译：低雷诺数的弧形Naca 65（1）-412翼型的直接数值模拟：流动分离，稳定性和拉格朗日空气动力学
6. Aerodynamic characteristics of NACA 4412 airfoil section with flap in extreme ground effect [O] . Alex E. Ockfen, Konstantin I. Matveev 2009

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Measurements of aerodynamic characteristics of a 35 degree sweptback NACA 65-009 airfoil model with 1/4-chord bevelled-trailing-edge flap and trim tab by the NACA wing-flow method

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