Hi,

i'm working for my final exam in aerodynamic and i spent a lot of time in a 3d panel code and a 2d unsteady code.

Now, i have to make the last work for the exam, a comparation between integral and finite difference method for laminar boundary layers, and i have only 6 days.

I'm lucky because these two codes are exactly INTGRL and BDYLAY in the Moran's book. I would know if someone has experience with these two codes, i.e. does they works? and, if not, do you know what are the drawbacks?

Thank you in advance

Paolo

sir

I need a written code for a panel method for a NACA four series aerofoil.

If you could do the above said then i will be grteatly obliged. thanking you in anticipation.

syed.