Air enters the afterburner nozzle of a jet fighter at 427°C with a velocity of 100 m/s. It leaves this adiabatic nozzle at 377°C. Assuming that the air specific heats do not change with temperature, the velocity at the nozzle exit is:A) 142 m/sB) 178 m/sC) 227 m/sD) 343 m/s
Already registered? Login
Not Account? Sign up
Enter your email address to reset your password
Back to Login? Click here