Air with a static temperature of 223 K entering a gas turbine engine intake at V1=300m/s accelerates to a new velocity (Vx) and decreases in pressure (P2) at the exit plane of the intake. The pressure recovery (P2/P1) through the intake is 0.833. Assume that the flow through the intake is isentropic.
(a) Calculate the static temperature (T2) of air exiting the intake
(b) Find the difference in total temperature (delta Tt) across the intake.
(c) Determine the velocity (V2) of the air exiting the intake.