$(30$ Points$)$ For an axial compressor stage : rotor, $23$ : stator$)T_{01}=290K,P_{01}=101\mathrm{.}3$kPa $M{a}_1=0\mathrm{.}7($on stationary reference$)$

Rotational. speed $=1000ra\frac{d}{s}$ Mean radius $=0\mathrm{.}3m$

${}_1=+40$

Mass flow rate $=22k\frac{g}{s}$

Total$-$to$-$total pressure ratio $=1\mathrm{.}3Aal$ speed remains constant.

Normal Design.

Ignore any losses.

Use $=1\mathrm{.}4$ and $R=287\frac{J}{k}gK.$

$($A$)$ Calculate all necessary quantities so that you can complete a table showing values of $T_0,T,P_0,P,Ma,C,C_z,C_{},W,W_{},,$ at $1,1R($on relative frame$),2$ R $($on relative frame$),$ and $2,$ and $3,$ as appropriate.

$($B$)$ Calculate stage loading coefficient, flow coefficient, reaction and stage power input.