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Showing results 1 to 7 of 7 Search took 0.00 seconds. Search: Posts Made By: hhh

Forum: FLUENT June 16, 2013, 05:47

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh Greetings bikalpa10 i didn't understand your... Greetings bikalpa10 i didn't understand your problem what is your domain size?

Forum: FLUENT August 18, 2012, 14:22

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in boundary condition Dear cfd seeker, i am doing steady analysis in for my 3D wing, for that i mesh in gambit & import in fluent. i consider solver is pressure based &my model is laminar flow, Know value i have is...

Forum: FLUENT August 7, 2012, 02:26

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in fluent Dear cfd seeker, thanks for your help.

Forum: FLUENT August 6, 2012, 03:51

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in fluent Dear cfd seeker, thanks, for your help, then which image i have to select and give velocity inlet,let me know.

Forum: FLUENT August 5, 2012, 02:40

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in fluent Dear cfd seeker, thanks for information, i know the definition of angle of attack, i already did 2D analysis of naca 0012, but 3D wing i dont know how to give boundary condition in fluent...

Forum: FLUENT August 4, 2012, 04:09

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in fluent Dear cfd seeker, thanks for your kind response, In fluent, For analysis of 2D naca0012 airfoil velocity inlet(boundary condition) we give vcostheta in x component & vsintheta in y component. ...

Forum: FLUENT August 3, 2012, 06:04

Replies: 14 3-D wing analysis problem Views: 3,427 Posted By hhh velocity inlet in fluent Dear friends, In fluent, For analysis of 2D naca0012 airfoil velocity inlet we give vcostheta in x component & vsintheta in y component, v is inlet velocity. 1)here i...

Showing results 1 to 7 of 7

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