Air enters a frictionless, constant area duct with Ma1 = 2.0,T0,1 = 59 F, and p0,1 =
Chapter 11, Problem 11.68(choose chapter or problem)
Air enters a frictionless, constant area duct with Ma1 = 2.0,T0,1 = 59 F, and p0,1 = 14.7 psia. The air is decelerated by heatinguntil a normal shock wave occurs where the local Mach number is 1.5. Downstream of the normal shock, the subsonic flow is acceleratedwith heating until it chokes at the duct exit. Determine thestatic temperature and pressure, the stagnation temperature andpressure, and the fluid velocity at the duct entrance, just upstreamand downstream of the normal shock, and at the duct exit. Sketchthe temperatureentropy diagram for this flow
Unfortunately, we don't have that question answered yet. But you can get it answered in just 5 hours by Logging in or Becoming a subscriber.
Becoming a subscriber
Or look for another answer