An engineer measures the flow velocity at the edges of a rectangular control volume (LxH) over a stationary flat wall (see figure). At edge A the velocity is uniform, directed in the horizontal direction, and with magnitude V...At edge C the horizontal component of the 377³ 197¹ 2375 7² + 16 where y = velocity is 41ý 16 while the vertical velocity has not been measured because it is not needed. At edge B the streamwise component of the velocity is constant and equal to V... while the vertical component is different from zero and must be accounted for. The flow is two dimensional, viscous, steady and incompressible with density 1047 kg/m³. Note that a value for the length of the wall L is not needed to solve this problem and that the pressure is uniform. Given that V. = 12 m/s and H= 0.02 m, determine The drag per unit span on the wall, D' = [ Give you answers to three significant digits. N/m

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An engineer measures the flow velocity at the edges of a rectangular control volume (LxH) over a stationary flat wall (see figure). At
edge A the velocity is uniform, directed in the horizontal direction, and with magnitude V... At edge C the horizontal component of the
197¹
2375
+
4
16
velocity is
41y
16
y² 37y³
4
, where y = 7, while the vertical velocity has not been measured because it
is not needed. At edge B the streamwise component of the velocity is constant and equal to V∞, while the vertical component is
different from zero and must be accounted for. The flow is two dimensional, viscous, steady and incompressible with density 1047
kg/m³. Note that a value for the length of the wall L is not needed to solve this problem and that the pressure is uniform. Given that V..
= 12 m/s and H= 0.02 m, determine
The drag per unit span on the wall, D' =
Give you answers to three significant digits.
A
N/m
B
L
D
C
H
Transcribed Image Text:An engineer measures the flow velocity at the edges of a rectangular control volume (LxH) over a stationary flat wall (see figure). At edge A the velocity is uniform, directed in the horizontal direction, and with magnitude V... At edge C the horizontal component of the 197¹ 2375 + 4 16 velocity is 41y 16 y² 37y³ 4 , where y = 7, while the vertical velocity has not been measured because it is not needed. At edge B the streamwise component of the velocity is constant and equal to V∞, while the vertical component is different from zero and must be accounted for. The flow is two dimensional, viscous, steady and incompressible with density 1047 kg/m³. Note that a value for the length of the wall L is not needed to solve this problem and that the pressure is uniform. Given that V.. = 12 m/s and H= 0.02 m, determine The drag per unit span on the wall, D' = Give you answers to three significant digits. A N/m B L D C H
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