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Temperature recovery factors on a slender 12 degree cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45 degrees

机译：温度恢复系数在细长的12度锥形圆柱体上，马赫数为3.0至6.3，攻角可达45度

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Reller, John O; Hamaker, Frank M;
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年度 1955
页码 1-59
总页数 59
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Investigation of the Magnus Effect of a Generic Projectile at Mach 3 Up to 16 Degrees Angle of Attack [J] . D. Klatt, R. Hruschka, F. Leopold Journal of Applied Mechanics: Transactions of the ASME . 2013,第3期

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2. Erosion mechanism of ternary-phase SiC/ZrB2-MoSi2-SiC ultra-high temperature multilayer coating under supersonic flame at 90 degrees angle with speed of 1400 m/s (Mach 4) [J] . Abdollahi Alireza, Valefi Zia, Ehsani Naser Journal of the European Ceramic Society . 2020,第4期

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3. Comparison of MRI, CT, Dunn 45 degrees and Dunn 90 degrees alpha angle measurements in femoroacetabular impingement [J] . Smith Kevin M., Gerrie Brayden J., McCulloch Patrick C., Hip international: the journal of clinical and experimental research on hip pathology and therapy . 2018,第4期

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4. INVESTIGATION OF THE MAGNUS EFFECT ON A GENERIC PROJECTILE AT MACH 3 UP TO 16 DEGREES ANGLE OF ATTACK [C] . D. Klatt, R. Hruschka, F. Leopold International symposium on ballistics . 2013

机译：在高达16度攻角的Mach 3上通用射弹的马格努球效应调查
5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Low-temperature damage and subsequent recovery of fab1 mutant Arabidopsis exposed to 2 degrees C. [O] . J Wu, J Lightner, N Warwick, 1997

机译：暴露于2°C的fab1突变拟南芥的低温损伤和随后的恢复。
7. Flowfield computations over the space shuttle Orbiter with a proposed canard at a Mach number of 5.8 and 50 degrees angle of attack [O] . Reuter William H. IV 1993

机译：马赫数5.8和迎角50度的拟议鸭形航天飞机Orbiter上的流场计算。

Temperature recovery factors on a slender 12 degree cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45 degrees

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