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Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54

机译：大型飞行测量的零升力阻力和低升力纵向特性的钻石翼体组合，马赫数从0.725到1.54

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Wallskog, Harvey A; Morrow, John D;
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年度 1953
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
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1. 大长径比带翼刚体的零升阻力系数和升力系数与马赫数的相关性（英文） [J] . 董素荣测试科学与仪器：英文版 . 2015 ,第003期
2. Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: theory and experiment [J] . Katsuyoshi Tanimizu, David J. Mee, Raymond J. Stalker, Shock Waves . 2009 ,第2期

机译：不同飞行马赫数下对准轴对称超燃冲压发动机的阻力：理论与实验
3. Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: theory and experiment [J] . Tanimizu K, Mee DJ, Stalker RJ, Shock Waves . 2009 ,第2期

机译：在各种飞行马赫数下对准轴对称超燃冲压发动机的拖曳力：理论和实验
4. Lift, drag and thrust at high flight Mach number [J] . Jack Pike Philosophical transactions of the Royal Society. Mathematical, physical, and engineering sciences . 1999 ,第1759期

机译：高飞行速度时的升力，阻力和推力
5. Estimating Zero-Lift Drag Coefficients and Maximum L/D in Subsonic Flight [C] . Pasquale M. Sforza AIAA aerospace sciences meeting;AIAA SciTech forum . 2018

机译：估算亚音速飞行中的零升降阻力系数和最大L / D
6. Optimal combination of number of participants and number of repeated measurements in longitudinal studies with time-varying exposure [O] . Jose Barrera-Gómez, Donna Spiegelman, Xavier Basagaña -1

机译：纵向研究中时变暴露的参与者人数和重复测量次数的最佳组合
7. Measurements of the pressure distributions on two circular cylinders of diameter d, vertically immersed in a turbulent boundary layer, are performed for various cylinder spacings s and angles of attack φ. The characteristics of the drag and lift forces acting on the cylinder are classified into three regions : i.e., 1) 0°＜__〜φ＜__〜30°, 2) 30°＜__〜φ＜__〜120°and 3) 120°＜__〜φ＜__〜180°which are divided by the two zero-lift force lines. Moreover, it is found that the interference between two cylinders is almost negligible for s/d＞__〜4, except for the influence of the wake region of the upstream cylinder. [O] . 谷口清一, 坂本弘志, Seiichi TANIGUCHI, 1980

机译：对于不同的气缸间距s和迎角φ，对垂直浸入湍流边界层的直径为d的两个圆柱上的压力分布进行测量。作用在气缸上的阻力和提升力的特性分为三个区域：1）0°＜__ 〜φ ＜__ 〜30°，2）30°＜__ 〜φ ＜__ 〜120°和3） 120°＜__ 〜φ ＜__ 〜180°除以两条零升力线。而且，发现除了上游气缸的尾流区域的影响之外，对于s / d＞ __〜4，两个气缸之间的干扰几乎可以忽略。

Large-scale flight measurements of zero-lift drag and low-lift longitudinal characteristics of a diamond-wing-body combination at Mach numbers from 0.725 to 1.54

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