[varunjain89]

hello all!

i'm writing my own CFD code for boundary layer eqns. over flat plate for laminar compressible flow, for mach no. 1.5... i'm using finite difference central-differencing scheme, and uniform grid spacing.... but the problem is, in order to stabilize the solution my deltaY=10^-8 and deltaX=10^-10, now even if i'm assuming a (5000,100)(x,y), practically my plate length is 5 x 10^-7, which is negligible.... can some one help me out, so that i can somehow increase my deltaX, and have a normal plate length.... if u want i can upload my code and graphs plotted....

thanks in advance
varun