cessation 发表于 2025-3-21 16:19:07
书目名称Numerical and Physical Aspects of Aerodynamic Flows影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0669255<br><br> <br><br>书目名称Numerical and Physical Aspects of Aerodynamic Flows读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0669255<br><br> <br><br>泰然自若 发表于 2025-3-21 23:27:59
Experiments on Initial and Boundary Conditionsntal interferences. Data obtained by the Wright brothers in their historic wind tunnel enabled them to evaluate the possibility of flying; by current standards they would probably not even fit in what engineers call the “ballpark” range. The designer’s problem is efficiency; errors larger than 1% inclarify 发表于 2025-3-22 03:57:54
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Some Observations on Numerical Solutions of the Three-Dimensional Navier-Stokes Equationsions. These flows may be either laminar or turbulent or both, and for laminar flow the use of the three-dimensional Navier-Stokes equations is required to adequately represent the motion. For turbulent flows, these same equations are usually ensemble-averaged, and with the introduction of current-ge无节奏 发表于 2025-3-22 20:20:38
Some Recent Studies in Triple-Deck Theorya continual challenge to theoreticians for many years. The usual approach, and one which I favor, is to regard it as controlled by an interaction between an external inviscid and a viscous boundary layer. For some time the discovery that a laminar boundary layer invariably appears to become siThymus 发表于 2025-3-23 00:24:28
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Nonasymptotic Theory of Unseparated Turbulent-Boundary-Layer — Shock-Wave Interactions with Applicat turbomachinery and air-breathing-engine inlets and diffusors. Of particular importance are the features of upstream influence, boundary-layer displacement, skin friction, and incipient separation dominated by the thin interactive shear-stress disturbance layer very close to the surface. Lighthill’scochlea 发表于 2025-3-23 06:12:24
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