Air is drawn into a small open-circuit vind tunnel as shown in Fig. Atmospheric oressure is 98.7 kPa (abs) and the temperature is 27 °C. If viscous effects are negligible, determine he pressure at the stagnation point on the nose of the airplane. Also determine the manometer reading, h, for the manometer attached to the static pressure tap within the test section of the vind tunnel if the air velocity within the test sec- ion is 50m/s.

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