|September 9, 2013, 23:30||
ansys14 fluent for airfoil
Join Date: Aug 2013
Posts: 37Rep Power: 5
I am working on 2D airfoil and trying to find the values for its Cd and Cl.I have to validate my result with a published work. But my results are not matching with the the paper.
Input values (same as paper):
SST model, Turbulence intensity to be 5%.
I did fluent analysis of S809 profile and found the Cl, Cd values for its validation.link for the paper: http://www.sciencedirect.com/science...96890412002634
For finding the Cd,Cl values:
Cd : report -> force -> X = x velocity, Y= y velocity.
Cl : report -> force -> X = -y velocity, Y= x velocity.
Please if anyone can help me out.
|Thread||Thread Starter||Forum||Replies||Last Post|
|heat transfer with RANS wall function, over a flat plate (validation with fluent)||bruce||OpenFOAM Running, Solving & CFD||6||January 20, 2017 07:22|
|Two questions on Fluent UDF||Steven||Fluent UDF and Scheme Programming||4||September 20, 2013 16:30|
|grid independence test in ansys14 fot fluent||abinashlipun||FLUENT||1||January 17, 2013 11:48|
|Alias problem when starting FLUENT from command line||batch_error||FLUENT||0||May 24, 2012 08:20|
|Problems in lauching FLUENT||Lourival||FLUENT||3||January 16, 2008 17:48|