1. Determine the maximum possible mass flow rate of air through a nozzle with a 1.00 × 10-3 m diameter throat and inlet stagnation conditions of 5.00 MPa and 30.0°C.
2. Determine the maximum flow rate of helium that passes through a nozzle with a 1.00 × 10-2 m diameter throat from an upstream stagnation state of 35.0 MPa at 27.0°C.