冠军
发表于 2025-3-21 18:26:32
书目名称New Results in Numerical and Experimental Fluid Mechanics XII影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0665735<br><br> <br><br>书目名称New Results in Numerical and Experimental Fluid Mechanics XII读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0665735<br><br> <br><br>
remission
发表于 2025-3-21 23:27:25
Unsteady Wake and Tailplane Loads of the Common Research Model in Low Speed Stallthe interaction of the separated wake with the tailplane in the presence of massively separated flow on the main wing. Validation of the CFD data using PIV data obtained for the flow conditions at ., . and . was carried out, confirming the generally satisfactory performance of the DDES simulations o
objection
发表于 2025-3-22 03:10:17
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共同确定为确
发表于 2025-3-22 05:33:54
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capsaicin
发表于 2025-3-22 11:45:38
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anticipate
发表于 2025-3-22 13:49:01
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contradict
发表于 2025-3-22 18:06:41
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相一致
发表于 2025-3-22 23:47:23
Modification of the SSG/LRR-, RSM for Turbulent Boundary Layers at Adverse Pressure Gradient with Sewhich was performed within the DLR project VicToria. We describe the design of the test case, the set-up in the wind-tunnel, and the measurement technique using particle imaging and particle tracking with the novel Shake-The-Box technique. We present the experimental results for the mean velocity pr
perpetual
发表于 2025-3-23 02:45:26
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下边深陷
发表于 2025-3-23 05:53:37
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