Question: CHAPTER 4 Basic Aerodynamics 4 . 2 0 A Pitot tube is mounted in the test section of a low - speed subsonic wind tunnel.

CHAPTER 4 Basic Aerodynamics
4.20 A Pitot tube is mounted in the test section of a low-speed subsonic wind tunnel.
The flow in the test section has a velocity, static pressure, and temperature of
150mih,1atm, and 70F, respectively. Calculate the pressure measured by the
Pitot tube.
CHAPTER 4 Basic Aerodynamics 4 . 2 0 A Pitot tube

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