作业
发表于 2025-3-21 18:12:18
书目名称New Results in Numerical and Experimental Fluid Mechanics V影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0665729<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics V读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0665729<br><br> <br><br>
inculpate
发表于 2025-3-21 21:12:41
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接合
发表于 2025-3-22 03:11:51
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slipped-disk
发表于 2025-3-22 05:10:31
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correspondent
发表于 2025-3-22 12:23:37
Application of the PSP Technique in Low Speed Wind Tunnelsipped with two propeller simulators driven by pressurized air. The great challenge was to compensate the influence of the warm and cold air pipes which are guided inside the wing, creating large temperature differences on the models surface. The PSP (pressure sensitive paint) measurements were carri
填满
发表于 2025-3-22 16:54:17
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monochromatic
发表于 2025-3-22 18:55:19
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cunning
发表于 2025-3-23 00:55:13
Aerodynamic Optimisation of a Flying Wing Transport Aircraftord length opfimisation. The applied finite volume flow solver is the DLR code FLOWer. The methods are described and results for a flying wing configuration are presented. The paper represents parts of DLR’s contribution to the aerodynamics work package of the VELA project, supported by European Com
分开
发表于 2025-3-23 03:12:31
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使长胖
发表于 2025-3-23 09:11:26
Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver test case is presented and compared to other numerical results. Having put the numerical method’s validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.