$($Show work and steps. Circle$/$box final answers$)$ Problem $2$

Air enters a constant$-$area channel at Mach $0\mathrm{.}4,$p$\_(1)=1\mathrm{.}0$atm, and T$\_(1)=300$K$.$ Inside the channel,

the heat added per unit mass is $10^(6)($J$)/($k$)$g$.$ Calculate the flow properties T$\_($O$\_(2)),$M$\_(2),$p$\_(2).$T$\_(2),$ and p$\_($O$\_(2))$

at the channel exit.

$10^(5)$