Consider the $2-$D inlet geometry as sketched below:

Assume inviscid flow. Find the conditions in region $2($after the oblique shock$)$:

P$2=?$

T$2=?$

M$2=?$

Find the axial force experienced by the internal solid walls of the inlet due to the fluid dynamics of the captured air$-$stream by:

a$.$ using the momentum equation $($relates axial force to exit and inlet fluid dynamics$)$

b$.$ using integration of actual pressure and shear forces on surfaces from inlet entrance $($i$)$ to inlet exit $($e$)(20$ pts $)$ Consider the $2-$D inlet geometry as sketched below:

standar

$M=3\mathrm{.}0$

$P=101$

$T=288K$

Assume inviscid flow. Find the conditions in region $2($after the oblique shock$)$:

$P_2=$

$T_2=$

$M_2=$

Find the axial force experienced by the internal solid walls of the inlet due to the fluid

dynamics of the captured air$-$stream by:

a$.$ using the momentum equation $($relates axial force to exit and inlet fluid dynamics$)$

b$.$ using integration of actual pressure and shear forces on surfaces from inlet entrance $($i$)$

to inlet exit $($e$)$