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An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.59

机译：对超音速飞机配置的研究，其具有带圆弧截面和40度后掠的锥形机翼：对机翼数为1.59的机翼的空气动力学特性进行压力分布研究

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Cooper, Morton; Spearman, M Leroy;
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年度 1950
页码 1-57
总页数 57
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations [J] . G. Q. Zhang, S. C. M. Yu, A. Chien, Journal of Aircraft . 2013,第2期

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3. Study the Influence of a Gap between the Wing and Slotted Flap over the Aerodynamic Characteristics of Ultra-Light Aircraft Wing Airfoil [J] . Cvetelina Velkova, Michael Todorov, Guillaume Durand 机械工程与自动化：英文版 . 2015,第005期

机译：研究机翼和缝隙襟翼之间的间隙对超轻型飞机机翼翼型气动特性的影响
4. Aerodynamic Investigations of an Advanced Over- the- Wing Nacelle Transport Aircraft Configuration [C] . G. Hill, O. Kandil AIAA Aerospace Sciences Meeting and Exhibit . 2007

机译：先进的越过机舱运输飞机配置的空气动力学研究
5. Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft Configuration. [D] . Kuntawala, Nimeesha B. 2011

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6. A Fundamental Study for Aerodynamic Characteristics of Supersonic Biplane Wing and Wing-Body Configurations [O] . Yusuke ODAKA, Kazuhiro KUSUNOSE 2009

机译：超音速双翼翼和翼形配置的空气动力学特性的基本研究

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.59

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