Part A

A jet plane is flying at $\backslash ($ M$=2\mathrm{.}4\backslash ),$ in air having a temperature of $\backslash (2^\{\backslash$circ$\}\backslash$mathrm$\{$C$\}\backslash )$ and absolute pressure of $80$ kPa $.$ The leading edge of the wing has an angle of $\backslash (\backslash$delta$=16^\{\backslash$circ$\}\backslash ).($Figure $1)$

Figure

$1$ of $1$

Determine the velocity of the air just in front or to the right of the oblique shock that forms on the wing.

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

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Part B

Determine the pressure of the air just in front or to the right of the oblique shock that forms on the wing.

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