A smooth netal sheet c Considered that there is no difference be tween - height) with 2 m' float ing with air flowing through the top ave a and bottom of the sheet when the air velocity above the plate is double of the air velocity below. Let the air dengity be equal to 1.2 kg/m³. Use the Beynoulli equation to find the pressure difference be tween the top bottom of the plate 1 and g = 10 m/s, air velocity at above is 12 m/s ) %D

College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
Publisher:Raymond A. Serway, Chris Vuille
Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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A
smooth netal sheet ( Considered that there is no difference be tween -
height) with
2 m?
float ing with air flowing through the top
ave a
and bottom
of the sheet
when the
ve locity above the plate
air
is double of the air velocity below.
Let the air demgity be equal to
kg/m³. Use the Bernoulli equation
1.2
to find the pressure difference be tween the top
and
bottom of the plate ?
9- 10 m/s,
air velocity at
above is
12 m/s )
%3D
Transcribed Image Text:A smooth netal sheet ( Considered that there is no difference be tween - height) with 2 m? float ing with air flowing through the top ave a and bottom of the sheet when the ve locity above the plate air is double of the air velocity below. Let the air demgity be equal to kg/m³. Use the Bernoulli equation 1.2 to find the pressure difference be tween the top and bottom of the plate ? 9- 10 m/s, air velocity at above is 12 m/s ) %3D
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