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140.5 MB |
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121.0 KB |
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1.3 GB |
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611.6 KB |
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8.5 GB |
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138.6 KB |
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8.5 GB |
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101.2 MB |
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9.9 GB |
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8.8 MB |
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30.0 MB |
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429.7 KB |
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SuicideGirls.com_14.10.15.Elfenlye.Fatally.Yours.XXX.IMAGESET-GAGBALL[rarbg] |
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142.4 MB |
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2.4 MB |
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6.0 GB |
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/ansys+workbench12官方教程/CFX_Intro_R12_Final/Workshops/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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928.7 KB |
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2.1 MB |
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/ansys+workbench12官方教程/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012.msh.gz |
1.2 MB |
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6.0 GB |
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/ansys+workbench12官方教程/CFX_Intro_R12_Final/Workshops/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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928.7 KB |
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2.1 MB |
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/ansys+workbench12官方教程/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012.msh.gz |
1.2 MB |
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274.9 MB |
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155.2 KB |
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12.7 GB |
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14.0 MB |
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/ANSYS CFX/ANSYS-CFX-Intro_13.0/input-files/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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3.3 MB |
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779.5 MB |
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/13_RE_Russia/FM+EPS/2013_RE_EURRUSSIA_WM/GRAPHIC/ACA00173AC00ENG.EPS |
140.5 KB |
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/13_RE_Russia/FM+EPS/2013_RE_EURRUSSIA_WM/GRAPHIC/ACA00117AC00ENG.EPS |
129.5 KB |
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78.3 KB |
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68.6 KB |
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701.4 MB |
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607.7 KB |
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/Примеры/Расчет обтекания профиля NACA0012 турбулентным сжимаемым потоком в Ansys.DOC |
607.7 KB |
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5.3 GB |
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/ANSYS-FLUENT-Intro_13.0_1st-ed_pdf/workshop-input-files/workshop2-airfoil-new/NACA0012.msh |
3.3 MB |
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5.5 GB |
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13.8 KB |
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81.0 KB |
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1.9 GB |
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/CFX_Intro_R12_Final/Workshops/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012-mach-0.5-conv.dat.gz |
2.1 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012.msh.gz |
1.2 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012-mach-0.5-conv.cas.gz |
928.7 KB |
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1.9 GB |
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/CFX_Intro_R12_Final/Workshops/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012-mach-0.5-conv.dat.gz |
2.1 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012.msh.gz |
1.2 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012-mach-0.5-conv.cas.gz |
928.7 KB |
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1.9 GB |
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/CFX_Intro_R12_Final/Workshops/02_Airfoil_Files/NACA0012.msh |
14.0 MB |
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2.1 MB |
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1.2 MB |
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/FLUENT_Intro_R12_Final/workshop-files/workshop02_airfoil/NACA0012-mach-0.5-conv.cas.gz |
928.7 KB |
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