mature
发表于 2025-3-21 17:20:04
书目名称Shear Flow in Surface-Oriented Coordinate影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0866519<br><br> <br><br>书目名称Shear Flow in Surface-Oriented Coordinate读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0866519<br><br> <br><br>
成绩上升
发表于 2025-3-21 21:53:10
Notes on Numerical Fluid Mechanics and Multidisciplinary Designhttp://image.papertrans.cn/s/image/866519.jpg
deficiency
发表于 2025-3-22 02:48:26
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看法等
发表于 2025-3-22 05:49:00
978-3-663-05277-7Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig 1981
凹槽
发表于 2025-3-22 09:27:50
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收集
发表于 2025-3-22 12:54:35
1612-2909 Overview: 978-3-663-05277-7978-3-663-05276-0Series ISSN 1612-2909 Series E-ISSN 1860-0824
PACK
发表于 2025-3-22 21:04:29
Boundary-Layer Parameters,propriate diagonal elements of the covariant metric tensor yields the physical coordinates of the shear stress tensor (see chapter 8). Here only the contributions relevant in zero- or first-order boundary-layer theory are given.
自然环境
发表于 2025-3-22 23:13:39
Initial Conditions for the Prediction of Boundary Layers on Wings and Fuselages, boundary-layer approach is not valid, for instance, for the flow along wing-fuselage junctions and along wing tips (see Fig. 6.1). The boundary-layer on portions of the aircraft, such as on wings or fuselages, can, however, be predicted quite well as long as the flow remains attached to the body surface.
开始没有
发表于 2025-3-23 04:49:54
Stagnation - Point Solution,urface, second-order boundary-layer effects are not taken into consideration. The recent studies of PAPENFUSS are concerned with second-order boundary layer effects at (nodal) points of attachment with strong suction or blowing.
去世
发表于 2025-3-23 06:06:26
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