Combustion gases with an average specific heat ratio of k=1.33
and a gas constant of R=0.280 kJ/kgK enter a 10-cm-diameter
adiabatic duct with inlet conditions of Ma1=2,21 T1=521 K, and P1
=182,1 kPa. If a normal shock occurs at a location 2021 mm from the
inlet, determine the velocity, temperature, and pressure at the
duct exit. Take the average friction factor of the duct to be
0.01021. Calculate the static stagnation pressure, temperature and
density values of the flow at...