b) A 4 m long and 2 m wide plate shown in Figure Q1(b) is positioned in seawater flowing at 1.5 m/s with p = 1025 kg and v= 1.004 X 10-6 m² m³ i) ii) iii) Determine the boundary layer thickness at the length of the plate. Draw the boundary layer by showing the thickness of the boundary layers in the laminar region and the turbulent region. Determine the friction drag acting on the plate's top side.

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Chapter5: Analysis Of Convection Heat Transfer
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b) A 4 m long and 2 m wide plate shown in Figure Q1(b) is positioned in seawater flowing
at 1.5 m/s with p = 1025
and v= 1.004 X 10-6
i)
ii)
Determine the boundary layer thickness at the
length of the plate.
Draw the boundary layer by showing the thickness of the boundary layers in the
laminar region and the turbulent region.
Determine the friction drag acting on the plate's top side.
V=1.5 m/s
m³
Property
Average skin friction
coefficient, Cr,x
Laminar
Figure Q1(b)
Cf.x²
4m
Turbulent
0.074
Re¹
1.33
Re, ¹/2
Re, 5 x 105 5 x 105 ReL ≤ 107
Cf.x
1/5
Mix flow
0.074 1742
REL
Re, ¹/5
5 x 105 Re≤ 107
Cf.x
Transcribed Image Text:b) A 4 m long and 2 m wide plate shown in Figure Q1(b) is positioned in seawater flowing at 1.5 m/s with p = 1025 and v= 1.004 X 10-6 i) ii) Determine the boundary layer thickness at the length of the plate. Draw the boundary layer by showing the thickness of the boundary layers in the laminar region and the turbulent region. Determine the friction drag acting on the plate's top side. V=1.5 m/s m³ Property Average skin friction coefficient, Cr,x Laminar Figure Q1(b) Cf.x² 4m Turbulent 0.074 Re¹ 1.33 Re, ¹/2 Re, 5 x 105 5 x 105 ReL ≤ 107 Cf.x 1/5 Mix flow 0.074 1742 REL Re, ¹/5 5 x 105 Re≤ 107 Cf.x
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