$\backslash$table$[[$Geometry $1,$Geometry $2],[\backslash$table$[[$Cylinder $($diameter $=8)],[$Velocity $=6$m$/$s$,$ angle of$],[$attack $=0$ deg, sea level$]],$NACA $4414]]$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.

Write according to the following geometries and flow conditions are given in the photos