Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.1 bar and inlet stagnation temperature of 310K. For an inlet Mach number of 0.80 and an inlet flow angle of 500, the exit flow angle is measured as 15.80. Assuming the flow is isentropic, determine the mass flow rate per unit frontal area, the exit Mach number and the static pressure ratio across the cascade.

! Required information NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Steam enters a converging nozzle at 5.0 MPa and 400°C with a negligible velocity, and it exits at 3.0 MPa. It has a nozzle exit area of 50 cm². Determine the exit velocity, mass flow rate, and exit Mach number if the nozzle is isentropic. The exit velocity is m/s. kg/s. The mass flow rate is The exit Mach number is

A converging-diverging nozzle is attached to a reservoir where the pressure is 718 kPa. The design exit Mach number is 2.9. What is the design exit pressure (in kPa)?