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.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Air is drawn into a small open-circuit
wind tunnel as shown in Fig. Atmospheric
pressure is 98.7 kPa (abs) and the temperature is
27 °C. If viscous effects are negligible, determine
the pressure at the stagnation point on the nose o
of the airplane. Also determine the manometer
reading, h, for the manometer attached to the
Test
Inlet nozzle, section
-Diffuser
Fan
(3)
Inlet
static pressure tap within the test section of the
wind tunnel if the air velocity within the test sec-
hLU Water
tion is 50 m/s.
Transcribed Image Text:Air is drawn into a small open-circuit wind tunnel as shown in Fig. Atmospheric pressure is 98.7 kPa (abs) and the temperature is 27 °C. If viscous effects are negligible, determine the pressure at the stagnation point on the nose o of the airplane. Also determine the manometer reading, h, for the manometer attached to the Test Inlet nozzle, section -Diffuser Fan (3) Inlet static pressure tap within the test section of the wind tunnel if the air velocity within the test sec- hLU Water tion is 50 m/s.
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