$\backslash$table$[[$Geometry $1,$Geometry $2],[\backslash$table$[[$Cylinder $($diameter $=9)],[$Velocity $=16$m$/$s$,$ angle of$],[$attack $=0$ deg, sea level$]],$NACA $2414]]$Write a $2-$D source panel method code which is described by J$.$D$.$ Anderson's in chapter $3\mathrm{.}17.$ The

code shall be written using MATLAB code. The panels points shall be inputted to the code with a

text file. When the code is executed, the flow conditions $($free stream velocity, angle of attack,

etc.$)$ shall be asked by the code. After the user define the conditions, the following outputs shall

be reported:

The accuracy of the numerical solution $($different panel numbers should be checked$),$

The pressure coefficients on the object and comparison with experimental or analytical

results,

Lift coefficient $($using Kutta$-$Joukowski theorem$)$ and compare with experimental or analytical

results.

All the studies and results shall be explained in a report. The report shall at least include:

The aim and the motivation of the study,

The Matlab codes shall be given in Appendix of the report,

and explanation of the calculations,

The discussion of the results.