灰尘
发表于 2025-3-21 19:29:03
书目名称Numerical and Phyical Aspects of Aerodynamic Flow III影响因子(影响力)<br> http://impactfactor.cn/if/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III影响因子(影响力)学科排名<br> http://impactfactor.cn/ifr/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III网络公开度<br> http://impactfactor.cn/at/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III网络公开度学科排名<br> http://impactfactor.cn/atr/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III被引频次<br> http://impactfactor.cn/tc/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III被引频次学科排名<br> http://impactfactor.cn/tcr/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III年度引用<br> http://impactfactor.cn/ii/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III年度引用学科排名<br> http://impactfactor.cn/iir/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III读者反馈<br> http://impactfactor.cn/5y/?ISSN=BK0669257<br><br> <br><br>书目名称Numerical and Phyical Aspects of Aerodynamic Flow III读者反馈学科排名<br> http://impactfactor.cn/5yr/?ISSN=BK0669257<br><br> <br><br>
调色板
发表于 2025-3-21 21:32:31
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Adornment
发表于 2025-3-22 02:43:41
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实现
发表于 2025-3-22 07:01:14
Transition Calculations in Three-Dimensional Flowss that initially infinitesimal disturbances, internalized by the boundary layer, are selectively amplified by the viscous flow as they propagate downstream. The amplification of a disturbance depends upon its frequency and propagation direction.
overrule
发表于 2025-3-22 09:20:36
The Computation of Viscid-Inviscid Interaction on Airfoils with Separated Flowe the boundary layers are thin and turbulent over most of the airfoil and wake. Our objective in this work is to develop a fast viscid-inviscid-interaction method that can compute viscous flows over airfoils with extensive regions of flow separation and that can be used to predict the stalling characteristics of airfoils with reasonable accuracy.
平息
发表于 2025-3-22 14:53:10
Laminar Separation Studied as an Airfoil Problemrfoils operating in the Reynolds-number (Re) range well below one million. This paper presents an aerodynamic theory of the laminar separation to further our understanding of the aerodynamic-flow behavior at Re = 10.–10., that is, at the lower end of this flight regime.
heartburn
发表于 2025-3-22 19:01:14
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chastise
发表于 2025-3-23 00:25:52
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协议
发表于 2025-3-23 04:04:34
Numerical and Phyical Aspects of Aerodynamic Flow III
Seizure
发表于 2025-3-23 06:14:01
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