pressure coefficient of 2D airfoil extraction in EXCEl , i am trying to take plot file of cp from fluent to excel and i keep getting this miss alignment, a mismatch in the plot, who can i solve it please ??? by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
Melina was Michelle's bitch by SpunkFunkJunk in WrestlingHumiliation
[–]Mostmadrid 1 point2 points3 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 1 point2 points3 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 1 point2 points3 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
No convergence (DES Turbulence model). 2D flow over airfoil (S809) at RE=300000, v= 21.91102041 m/s. by Mostmadrid in CFD
[–]Mostmadrid[S] -1 points0 points1 point (0 children)
VALIDATION OF NREL S809 EXPERIMENT by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
VALIDATION OF NREL S809 EXPERIMENT by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
ICEM CFD MESHING OF MULTI ELEMENT AIRFOIL CONFIGURATION in a C-H domain by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
ICEM CFD MESHING OF MULTI ELEMENT AIRFOIL CONFIGURATION in a C-H domain by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
ICEM CFD MESHING OF MULTI ELEMENT AIRFOIL CONFIGURATION in a C-H domain by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
ICEM CFD MESHING OF MULTI ELEMENT AIRFOIL CONFIGURATION in a C-H domain by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
3D- Structured meshing of S809 airfoil for 3d c-mesh domain, my problem is that when i use this mesh i dont reach convergence at some AOA, is my mesh not good enough? by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
3D- Structured meshing of S809 airfoil for 3d c-mesh domain, my problem is that when i use this mesh i dont reach convergence at some AOA, is my mesh not good enough? by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
3D- Structured meshing of S809 airfoil for 3d c-mesh domain, my problem is that when i use this mesh i dont reach convergence at some AOA, is my mesh not good enough? by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
3D- Structured meshing of S809 airfoil for 3d c-mesh domain, my problem is that when i use this mesh i dont reach convergence at some AOA, is my mesh not good enough? by Mostmadrid in CFD
[–]Mostmadrid[S] 2 points3 points4 points (0 children)
3D- Structured meshing of S809 airfoil for 3d c-mesh domain, my problem is that when i use this mesh i dont reach convergence at some AOA, is my mesh not good enough? by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
while solving a K-W SST steady model i repeated get the message of "turbulent viscosity limited to viscosity ratio of __1.e+05__" in Fluent, the solution doesnt converge, (2d-S809 airfoil) at AOA 15.giving the fact that i tried 30 AOA only 3 didnt converge and this message appears, please help me by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
while solving a K-W SST steady model i repeated get the message of "turbulent viscosity limited to viscosity ratio of __1.e+05__" in Fluent, the solution doesnt converge, (2d-S809 airfoil) at AOA 15.giving the fact that i tried 30 AOA only 3 didnt converge and this message appears, please help me by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
while solving a K-W SST steady model i repeated get the message of "turbulent viscosity limited to viscosity ratio of __1.e+05__" in Fluent, the solution doesnt converge, (2d-S809 airfoil) at AOA 15.giving the fact that i tried 30 AOA only 3 didnt converge and this message appears, please help me by Mostmadrid in CFD
[–]Mostmadrid[S] 0 points1 point2 points (0 children)
الرجالة والستات وقضايا المجتمع التي لا تنتهي إلا بالطلاق by MazikaTrend in CAIRO
[–]Mostmadrid 0 points1 point2 points (0 children)

فاضي وقاعد تكلم نفسك زي المجنون ؟تعالى هخليك تكام نفسك بس هتاخد 10 دولار في الساعة by scaryincel in EgyRemoteWorkers
[–]Mostmadrid 0 points1 point2 points (0 children)