- #1
kronecker77
- 10
- 0
I am given a project to transform an airfoil from a cylinder using joukowski transform. The cylinder is in zeta plane and the airfoil is in z plane. I did the plotting and i got the airfoil shape using matlab. but i want to know how to plot the pressure distribution over the airfoil.
The inputs to my program are:
Velocity, Angle of attack, coordinates of center of circle(zeta plane), radius of circle(zeta plane).
Can somebody please tell me how to plot pressure distribution for an airfoil?
I am using Matlab to do the stuff but i m getting weird plots for pressure distribution. Please help me of someone can...deadline near
The inputs to my program are:
Velocity, Angle of attack, coordinates of center of circle(zeta plane), radius of circle(zeta plane).
Can somebody please tell me how to plot pressure distribution for an airfoil?
I am using Matlab to do the stuff but i m getting weird plots for pressure distribution. Please help me of someone can...deadline near