Question 1:
Write down the different types of panels which are employed in the analysis of flow using panel method.
Question 2:
Illustrate out in detail about source panel method.
Question 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.
Question 4:
Using vortex panel technique, acquire the lift generated by the flat plate considering N vortex panels. Make essential suppositions.
Question 5:
In brief write about shock fitting and shock capturing methods using neat and proper sketches. Illustrate how shock capturing method is employed for conserved form of equations.
Question 6:
Write down a brief notes on
a) Stability
b) Consistency
c) Lax-equivalence theorem
d) Round-off and discrimination errors.
Question 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.
Question 8:
Write down the theoretical characteristics of transonic flows.