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Exploratory investigation at high and low subsonic Mach numbers of two experimental 6-percent-thick airfoil sections designed to have high maximum lift coefficients

机译：两个实验6％厚翼型截面的高低亚音马赫数的探索性研究，设计具有较高的最大升力系数

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Loftin, Laurence K , Jr; Von Doenhoff, Albert E;
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年度 1951
页码 1-51
总页数 51
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:20:00

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2. EXPERIMENTAL DETERMINATION OF THE INFLUENCE OF TURBULENT SCALE ON THE LIFT AND DRAG COEFFICIENTS OF LOW REYNOLDS NUMBER AIRFOILS [J] . J.S.DELNERO, J.MARANON DI LEO, F.A.BACCHI, Latin American Applied Research . 2005,第3期

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4. Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3- element high-lift wing sections [C] . J. Wild AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2012

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5. Determination of forced convective heat transfer coefficients for subsonic flows over heated asymmetric NANA 4412 airfoil. [D] . Dag, Yusuf. 2013

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7. Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections [O] . Jochen Wild 2012

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Exploratory investigation at high and low subsonic Mach numbers of two experimental 6-percent-thick airfoil sections designed to have high maximum lift coefficients

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