[quickzotic]

I have no knowledge about CFD programing. Just I am good at using of software like FLUENT or CFX. But I got a HMW about this title. If I don't get it, probably I will fail from class. So it is very important for me. I need matlab code or fortran(it doesn't matter) within flow over cylinder(or airfoil ) using method of source panel. The specifications ; It should be demonstrated source strength, velocity, pressure coefficent distribution wtih tables and graphs on object surface. And also it must calculated total source srtegth and total drag. Also It is wanted to use Ii,j integration formulation in the program.
If somebody helps I will appreciate.