(Solved): A static thrust stand as sketched is to be designed for testing a jet engine. The following conditi ...

A static thrust stand as sketched is to be designed for testing a jet engine. The following conditions are known for a typical test: Intake air velocity $V_1=200\frac{\mathrm{m}}{\mathrm{s}}$; exhaust gas velocity $V_2=500\frac{\mathrm{m}}{\mathrm{s}}$; intake crosssectional area $A_1=1\mathrm{m}$; intake static pressure $p_1=?22.5=78.5\mathrm{kPa}(abs)$; intake static temperature $T_1=268\mathrm{K}$; exhaust static pressure $p_2=0\mathrm{kPa}=101\mathrm{kPa}(abs)$; exhaust static temperature $T_2=$ $300\mathrm{K}$. Specific gas constant $R=287\frac{1}{\mathrm{kg}K}$ Estimate the nominal anchoring force for which to design. Extra credit. Find the design area $A_2$.