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Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method

机译：通过NaCa翼流法测试的跨音速下6％厚对称双楔翼型的空气动力学特性

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Lina, Lindsay J;
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年度 1949
页码 1-30
总页数 30
原文格式 PDF
正文语种 eng
中图分类工业技术;
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5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

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6. Aerodynamics of a highly irregular body at transonic speeds—Analysis of STRATOS flight data [O] . Markus Guerster, Ulrich Walter 2011

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Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method

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