Numerical vortex panel method for lifting flows over an airfoil.
I am having some diffuculty running my program in fortran. it is rather unpredictible and the results that generated from the program are unstable with results converges and divereges from ideal result. so if there is anyone out there who has a program on numerical vortex panel method (with constant vortex distribution along the panels) then please get in contact with. Much appreciated
We are undergraduate students of regional engg college ,silchar,india.we have very little knowledge on CFD ,and would like to know more .So please send us some info on this topic.thank u.
|All times are GMT -4. The time now is 09:09.|