1. A 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 150 rnilh, 1 atm, and 70°F, respectively. Calculate the pressure measured by the tube. 2. The altimeter on a low-speed Piper Aztec reads 8000 ft. A tube mounted on the wing tip measures a pressure of 1650 /ft2. If the outside air temperature is 500°R, what is the true velocity of the airplane? What is the equivalent airspeed?

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