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onsider a Venturi with a throat-to-inlet area ratio of 0.8, mounted on the side of an airplane fuselage. The airplane is in flight at standard sea level. If the static pressure at the throat is 2100 lb/ft3,
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onsider a Venturi with a throat-to-inlet area ratio of 0.8, mounted on the side of an airplane fuselage. The airplane is in flight at standard sea level. If the static pressure at the throat is 2100 lb/ft3, calculate the velocity of the airplane. Note that standard sea level density and pressure are 1.23 kg/m3 (0.002377 slug/ft3) and 1.01 x 105 N/m2 (2116lb/ft3), respectively.

User Jaquann
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1 Answer

4 votes

Answer:

= 154.70ft/s

Step-by-step explanation:

see the attached file

onsider a Venturi with a throat-to-inlet area ratio of 0.8, mounted on the side of-example-1
User Skytaker
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