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Search: Posts Made By: mahzad
Forum: Main CFD Forum August 6, 2012, 03:36
Replies: 13
Views: 9,425
Posted By mahzad
Hi, my problem was not with the calculation of...

Hi, my problem was not with the calculation of Cp, I just didn't know is it correct to use P_out instead of p_infinity for calculation of Cp or not. because in books P_infinity is referred to...
Forum: Main CFD Forum August 5, 2012, 10:56
Replies: 13
Views: 9,425
Posted By mahzad
My grid is completely structured, and so it would...

My grid is completely structured, and so it would take me a long time specially for unsteady modeling.Anyway thanks, I'm deeply grateful to you for your help dear! your information was really helpful...
Forum: Main CFD Forum August 5, 2012, 09:46
Replies: 13
Views: 9,425
Posted By mahzad
ok thanks, another question is that when my...

ok thanks, another question is that when my solution reach a steady state condition, the pressure is not exactly 1 at inlet, it's for example 1.12 and also it is not 1.12 at every node on inlet...
Forum: Main CFD Forum August 5, 2012, 08:02
Replies: 13
Views: 9,425
Posted By mahzad
So you mean that, in case of any differences I...

So you mean that, in case of any differences I can add (p_out-p_in)/(rho*V^2/2) to the Cp values over the airfoil surface?
Forum: Main CFD Forum August 5, 2012, 06:43
Replies: 13
Views: 9,425
Posted By mahzad
I know that this shift doesn't have any effect on...

I know that this shift doesn't have any effect on lift or drag, but I am comparing my pressure coefficient results. So a shift matters here. My problem is that, because the flow is viscous and low...
Forum: Main CFD Forum August 5, 2012, 01:20
Replies: 13
Views: 9,425
Posted By mahzad
I checked this book, in chapter 8 of this book...

I checked this book, in chapter 8 of this book the method which must be used to set the boundary condition at inlet or outlet for subsonic or supersonic flow is explained! it is not my question?!!! I...
Forum: Main CFD Forum August 4, 2012, 13:55
Replies: 13
Views: 9,425
Posted By mahzad
calculating pressure coefficient on airfoil surface

Hi every one I am modeling an airfoil in an incompressible low Re flow! I set pressure in my outlet boundary condition as 1. I also set velocity in x and y direction at inlet. my question is when I...
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