Air enters a converging-diverging nozzle at a stagnation pressure of 2mpa, a stagnation temperature of 400k, and a mach number of 0.5. the flow is accelerated isentropically through the nozzle to a mach number of 4(station x), passes through a normal shock (x to y), and then flows isentropically to the exit. given a nozzlethroat area of 0.05m2 and exit area of 1m2, find the location of the shock (nozzle area).

Two flowing streams of argon gas are adiabatically mixed to form a single flow/stream. one stream is 1.5 kg/s at 400 kpa and 200 c while the second stream is 2kg/s at 500 kpa and 100 ? . it is stated that the exit state of the mixed single flow of argon gas is 150 c and 300 kpa. assuming there is no work output or input during the mixing process, does this process violate either the first or the second law or both? explain and state all your assumptions.

Along 8-cm diameter steam pipe whose external surface temperature is 900c connects two buildings. the pipe is exposed to ambient air at 70c with a wind speed of 50 km/hr blowing across the pipe. determine the heat loss from the pipe per unit length. (b) air at 500c enters a section of a rectangular duct (15 cm x 20 cm) at an average velocity of 7 m/s. if the walls of the duct are maintained at 100c. a) the length of the tube for an exit temperature of the air to be 40 0c. b)the rate of heat transfer from the air. c) the fan power needed to overcome the pressure drop in this section of the duct.

Apressure vessel with an r/t 20 cannot be treated as thin walled vessel. a)-trune b)- false