|
[Sponsors] |
![]() |
![]() |
#1 |
New Member
Join Date: Apr 2009
Posts: 26
Rep Power: 16 ![]() |
Ok. I have this problem here. I am using AVL Swift for my simulation for airfoil project. The results i have are only velocity in the x and y direction and pressure.
The lift force i know could be calculated using the pressure values over the aifoil surface. How do i go about finding the drag force(wall shear stress and pressure drag) on the airfoil to find my Cd data using only those values. Any help would do. Would also like to know more about how the drag force is calculated in wind tunnels. Thanks alot. |
|
![]() |
![]() |
![]() |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Drag and lift force using OpenFoam14 | hardy | OpenFOAM Running, Solving & CFD | 26 | March 21, 2013 04:17 |
how to set lift and drag coefficients in force mon | alagesanj | FLUENT | 0 | November 16, 2008 20:47 |
Drag & lift force | Max | CFX | 1 | September 4, 2008 11:41 |
finding drag and lift force | Deloat | CFX | 3 | February 27, 2008 16:53 |
Lift and Drag force | Dmitriy | CFX | 4 | September 18, 2005 01:00 |