problem 1:

prepare down the different types of panels which are employed in the analysis of flow using panel method.

problem 2:

Illustrate out in detail about source panel method.

problem 3:

Illustrate out the term isentropic flow. What do you understand by quasi-one dimensional flow and derive expressions for governing equations of the quasi-one dimensional steady, isentropic flow by considering equation of state.

problem 4:

Using vortex panel technique, acquire the lift generated by the flat plate considering N vortex panels. Make essential suppositions.

problem 5:

In brief prepare about shock fitting and shock capturing methods using neat and proper sketches. Illustrate how shock capturing method is employed for conserved form of equations.

problem 6:

prepare down a brief notes on

a) Stability

b) Consistency

c) Lax-equivalence theorem

d) Round-off and discrimination errors.

problem 7:

Illustrate out with the aid of the schematic diagram the design procedure for nozzle contour employed in supersonic wind tunnels by the technique of characteristics.

problem 8:

prepare down the theoretical characteristics of transonic flows.