Air flows at $\backslash (700\backslash$mathrm$\{$~m$\}/\backslash$mathrm$\{$s$\}\backslash )$ through a long duct in a wind tunnel, where the temperature is $\backslash (15^\{\backslash$circ$\}\backslash$mathrm$\{$C$\}\backslash )$ and the absolute pressure is $60$ kPa $.$ The leading edge of a wing in the tunnel is represented by the $\backslash (8^\{\backslash$circ$\}\backslash )$ wedge. The angle of attack is set at $\backslash (\backslash$alpha$=1\mathrm{.}5^\{\backslash$circ$\}\backslash ).($Figure $1)$

Part A

Determine the pressure created on its top surface.

Express your answer to three significant figures and include the appropriate units.

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