Question: Problem 1 ( 2 0 Points ) : Consider the shape shown, which resembles a NACA 0 0 1 5 airfoil. Analyze the following shape

Problem

1 (20

Points

)

: Consider the shape shown, which resembles a NACA

0015

airfoil. Analyze the following shape using source panel method. Let each panel have a uniform strength and number the panels as shown in the figure. Please show intermediate steps so that partial credit can be assigned.

.

Find

(

) / (

_(\

infty

))

for each panel.

.

Determine

(

_(

)) / (

_(\

infty

))

for each panel.

.

Find C

_(

)

for each panel.

Problem 1 ( 2 0 Points ) : Consider the shape

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