Air is streaming past a horizontal air plane wing such that its speed is 120 m/s over the upper surface and 90 m/s at the lower surface. If the density of air is 1-3 kg/m^3. Find the difference in the pressure between the top and the bottom of the wing. If the wing is 10.0 m long and has an average width of 2.0 m, then find the gross lift of the wind on air plane.

Physics for Scientists and Engineers: Foundations and Connections
1st Edition
ISBN:9781133939146
Author:Katz, Debora M.
Publisher:Katz, Debora M.
Chapter15: Fluids
Section: Chapter Questions
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Air is streaming past a horizontal
air plane wing such that its
speed is 120 m/s over the upper
surface and 90 m/s at the lower
surface. If the density of air is
1-3 kg/m^3. Find the difference
in the pressure between the top
and the bottom of the wing. If the
wing is 10.0 m long and has an
average width of 2.0 m, then find
the gross lift of the wind on air
plane.
Transcribed Image Text:Air is streaming past a horizontal air plane wing such that its speed is 120 m/s over the upper surface and 90 m/s at the lower surface. If the density of air is 1-3 kg/m^3. Find the difference in the pressure between the top and the bottom of the wing. If the wing is 10.0 m long and has an average width of 2.0 m, then find the gross lift of the wind on air plane.
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