A wind tunnel using air is designed to have a Mach number of 3, a static pressure of 1.5
Chapter 12, Problem 12.48(choose chapter or problem)
A wind tunnel using air is designed to have a Mach number of 3, a static pressure of 1.5 psia, and a static temperature of - I 0F in the test section. Determine the area ratio of the nozzle required and the reservoir conditions that must be maintained if air is to be used.
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