Air at Mach 1.8 at an altitude of 8 km ISA, passes through anormal shockwave.
a) Calculate the velocity of the flow in units of metres persecond after the shock wave.
b) Calculate the change in specific entropy across theshockwave. Make sure you
include the appropriate units in your answer.
Join us to gain access to millions of questions and expert answers. Enjoy exclusive benefits tailored just for you!
(Save $1 )
One time Pay
(Save $5 )
Billed Monthly
*First month only
You can see the logs in the Dashboard.