State and illustrate divergence theorem for the vector field.
Develop the continuity equation for the fluid flow in the form of partial differential equation.
Illustrate a doublet and derive the expression for stream function in doublet flow.
Develop the expression for non-lifting flow over the circular cylinder.
Develop the expression for the momentum thickness in the boundary layer.
Illustrate out thermal boundary layer and with the use of sketches, illustrate the temperature variations in boundary layer.
Demonstrate schematically the pressure variation over airfoil at a high angle of attach (say, 25 degrees) and illustrate the causes.