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Drag measurements of symmetrical circular-arc and NACA 65-009 rectangular airfoils having an aspect ratio of 2.7 as determined by flight tests at supersonic speeds

机译：拖曳测量对称圆弧和NaCa 65-009矩形翼型，纵横比为2.7，由超音速飞行试验确定

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Alexander, Sidney R;
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年度 1947
页码 1-11
总页数 11
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Drag of an Airfoil in Accelerated, Supersonic Flight [J] . Journal of Applied Physics . 1948,第12期

机译：加速超音速飞行中的机翼阻力
2. Lift-to-Drag Ratio of a NACA0012 Airfoil in a Periodic Flow for Changing Angle of Attack [J] . Yu SHIBATA, Yohsuke TANAKA, Yoshitaka ISODA, Advanced Experimental Mechanics . 2019,第3期

机译：改变迎角的周期性流动中NACA0012机翼的升阻比
3. OPTIMIZATION OF THE SLOT SUCTION OF AIR FROM A CIRCULAR VORTEX CELL ON A THICK NACA0022 AIRFOIL WITH A MAXIMUM LIFT-DRAG RATIO [J] . S. A. Isaev, E. I. Kalinin, A. G. Sudakov, Journal of engineering physics and thermophysics . 2015,第6期

机译：优化具有最大升降比的厚NACA0022机翼上圆形涡流细胞的吸入空气
4. Aerodynamic Design of Biplane Airfoils for Low Wave Drag Supersonic Flight [C] . D. Maruyama, K. Matsushima, K. Kusunose, 24th Applied Aerodynamics Conference . 2006

机译：低波阻力超音速飞行的双翼机翼气动设计
5. BASE DRAG EFFECTS ON MAXIMUM LIFT-TO-DRAG RATIO AIRFOILS AT MODERATE SUPERSONIC SPEEDS [D] . PRITCHARD, ROBERT EMLYN -1

机译：在中等超声速下最大升降比比翼型上的基本拉力效应
6. Moving Model Test of High-Speed Train Aerodynamic Drag Based on Stagnation Pressure Measurements [O] . Mingzhi Yang, Juntao Du, Zhiwei Li, -1

机译：基于停滞压力测量的高速列车气动阻力运动模型试验
7. BASE DRAG EFFECTS ON MAXIMUM LIFT-TO-DRAG RATIO AIRFOILS AT MODERATE SUPERSONIC SPEEDS [O] . PRITCHARD, ROBERT EMLYN 1970

机译：在中等超声速下最大升降比比翼型上的基本拉力效应

Drag measurements of symmetrical circular-arc and NACA 65-009 rectangular airfoils having an aspect ratio of 2.7 as determined by flight tests at supersonic speeds

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