prepare down the different types of panels which are employed in the analysis of flow using panel method.
Illustrate out in detail about source panel method.
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.
Using vortex panel technique, acquire the lift generated by the flat plate considering N vortex panels. Make essential suppositions.
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.
prepare down a brief notes on
c) Lax-equivalence theorem
d) Round-off and discrimination errors.
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.
prepare down the theoretical characteristics of transonic flows.