problem 1:
State and illustrate divergence theorem for the vector field.
problem 2:
Develop the continuity equation for the fluid flow in the form of partial differential equation.
problem 3:
Illustrate a doublet and derive the expression for stream function in doublet flow.
problem 4:
Develop the expression for non-lifting flow over the circular cylinder.
problem 5:
Develop the expression for the momentum thickness in the boundary layer.
problem 6:
Illustrate out thermal boundary layer and with the use of sketches, illustrate the temperature variations in boundary layer.
problem 7:
Demonstrate schematically the pressure variation over airfoil at a high angle of attach (say, 25 degrees) and illustrate the causes.