$6$

Problem $04\mathrm{.}012-$ Calculate flow velocity of a supersonic transport

$10$

points

A supersonic transport is flying at a standard altitude of $50,000ft$ with a velocity of $1500\mathrm{.}250m\frac{i}{h}.$ The temperature at a point in the flow over the wing is $793\mathrm{.}32.$ Calculate the flow velocity at that point. For air, $\{$:$c_p=6000ft*\frac{b}{(slug)R})$ The flow velocity is $|f\frac{t}{s}.$