关税
发表于 2025-3-21 17:40:10
书目名称New Results in Numerical and Experimental Fluid Mechanics影响因子(影响力)<br> http://impactfactor.cn/if/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics影响因子(影响力)学科排名<br> http://impactfactor.cn/ifr/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics网络公开度<br> http://impactfactor.cn/at/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics网络公开度学科排名<br> http://impactfactor.cn/atr/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics被引频次<br> http://impactfactor.cn/tc/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics被引频次学科排名<br> http://impactfactor.cn/tcr/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics年度引用<br> http://impactfactor.cn/ii/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics年度引用学科排名<br> http://impactfactor.cn/iir/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics读者反馈<br> http://impactfactor.cn/5y/?ISSN=BK0665724<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics读者反馈学科排名<br> http://impactfactor.cn/5yr/?ISSN=BK0665724<br><br> <br><br>
Climate
发表于 2025-3-21 20:32:05
Density Measurements on a Delta Wing by Means of Planar Intensity Distribution of Rayleigh Scatteredences made during these first tests, the quantitative determination of the density field above a delta wing has been performed at Mach numbers between 0.5 and 1.4 in the transonic wind tunnel (TWG) of the DLR Göttingen. Three dimensional density fields with a resolution of about 1% have been obtained.
Deceit
发表于 2025-3-22 03:14:54
Numerical and Experimental Investigations of Flow Induced by Harmonic Motion of a Circular Cylindernder in water at rest at Reynolds number Re=100 and Keulegan-Carpenter number KC=5 was computed accurately in time. Computations have been performed applying different grid levels and time steps. Stable, symmetric and periodic flow patterns occurred showing good agreement with time averaged LDA measurements providing phase resolution of 1 degree.
anaerobic
发表于 2025-3-22 07:48:37
Alternative drag calculations from off body flow quantities using the FLOWer codeentional surface force integration techniques. The method is applied to two-dimensional flow field solutions obtained from the FLOWer code. Qualitative comparisons of the two techniques are presented for a NACA 0012 airfoil at different Mach numbers.
种植,培养
发表于 2025-3-22 09:41:07
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Commentary
发表于 2025-3-22 15:55:54
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变化
发表于 2025-3-22 19:08:07
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bifurcate
发表于 2025-3-22 23:43:33
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contrast-medium
发表于 2025-3-23 02:02:49
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nonchalance
发表于 2025-3-23 07:44:12
Reduction of Aerodynamic Drag (RaWid) in the national Research and Technology Programme for Aeronautlogies required for a MEGALINER which gains momentum by the ambitious plans for a new large Airbus A3XX..In the first year new technological steps were undertaken in theory, design and experiment. Some critical steps were verified by wing designs checked in wind tunnel tests.