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Wind-tunnel investigation of an NACA 23012 airfoil with a Handley Page slat and two flap arrangements

机译：使用Handley page板条和两个襟翼布置的NaCa 23012翼型的风洞调查

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作者
Schuldenfrei, Marvin J;
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年度 1942
页码 1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORDINATES - WING SLATS, HANDLEY; AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORDINATES - WING FLAPS, SPLIT; AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORDINATES - WING FLAPS, SLOTTED; AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORDINATES - WING SLOTS & FLAPS,; AIRFOILS - NACA 23012 - CHAR , A C , MOMENTS & ORDINATES - WING SLOTS & FLAPS,;

机译：aIRFOILs - NaCa 23012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - WING sLaTs，HaNDLEY; aIRFOILs - NaCa 23012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - WING FLaps，spLIT; aIRFOILs - NaCa 23012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - WING FLaps，sLOTTED; aIRFOILs - NaCa 23012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - WING sLOTs＆amp;皮瓣,; aIRFOILs - NaCa 23012 - CHaR，a C，mOmENTs＆amp; ORDINaTEs - WING sLOTs＆amp;皮瓣,;

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1. Experimental investigation of the dynamic stall phenomenon on a NACA 23012 oscillating airfoil [J] . Alex Zanotti, Giuseppe Gibertini Proceedings of the Institution of Mechanical Engineers . 2013,第G9期

机译：NACA 23012翼型动静失速现象的实验研究
2. Feedback control of laminar flow separation on NACA23012 airfoil by POD analysis and using perturbed Navier-Stokes equations [J] . Zare A., Emdad H., Goshtasbirad E. International Journal for Numerical Methods in Fluids . 2018,第4期

机译：通过POD分析和使用扰动Navier-Stokes方程，在Naca23012翼型上的层流分离的反馈控制
3. Simulation Of Flow Over NACA 23012 Airfoil In Incompressible And Compressible Subsonic Regimes [J] . V.Guru Shanker, V.Siva Rama Krishna, K. Chandra Shekar International journal of chemistry and applications . 2016,第1期

机译：不可压缩和可压缩亚音速状态下NACA 23012翼型流动的模拟
4. Analyzing a NACA 23012 Airfoil Composed of a Double-Slotted Fowler Flap and a Leading-Edge Handley-Page Slat with the Use of Computational Fluid Dynamics [C] . Aaron Glaser, Shigeo Hayashibara General Aviation Technology Conference and Exhibition . 2007

机译：分析NACA 23012翼型组成，由双槽圈襟翼组成和使用计算流体动力学的前沿围栏板基板组成
5. Experimental Investigation of Stall Cells on NACA0015 Airfoils [D] . Dell'Orso, Haley. 2017

机译：NACA0015机翼上失速细胞的实验研究
6. Correction: CFD study on NACA 4415 airfoil implementing spherical and sinusoidal Tubercle Leading Edge [O] . S. M. A. Aftab, K. A. Ahmad 2011

机译：校正：使用球形和正弦形结核前缘的NACA 4415机翼的CFD研究
7. Analisa Aerodinamika Flap Dan Slat Pada Airfoil Naca 2410 Terhadap Koefisien Lift Dan Koefisien Drag Dengan Metode Computational Fluid Dynamic [O] . Hartanto Tri 2015

机译：用计算流体动力学方法分析Naca 2410翼型襟翼和翼板的升力系数和阻力系数的气动分析。

Wind-tunnel investigation of an NACA 23012 airfoil with a Handley Page slat and two flap arrangements

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