ME $341$ FLUID MECHANICS ASSIGNMENT $1$

A static thrust stand is to be designed for testing a specific jet engine. Knowing the following conditions for a typical test, estimate a nominal thrust to design for. $(R=287\frac{J}{k}g.)$

intake air velocity $=214\frac{m}{s}$

exhaust gas velocity $=500\frac{m}{s}$

intake cross section area $=0\mathrm{.}93m^2$

intake static pressure $=-22\mathrm{.}7$kPa,$78\mathrm{.}6kP\frac{a}{a}bs$

SHOW ALL THE STEPS OF SOLUTION $!!!$