Solve Problem 9.13 with the velocity profile at section bc given by the parabolic expression from Problem 9.8. 9.13 A fluid, with density ρ = 1.5 slug/ft 3 , flows at U = 10 ft/s over a flat plate 10 ft long and 3 ft wide. At the trailing edge, the boundary-layer thickness is δ = 1 in. Assume the velocity profile is linear, as shown, and that the flow is two-dimensional (flow conditions are independent of z ). Using control volume abcd , shown by the dashed lines, compute the mass flow rate across surface ab . Determine the drag force on the upper surface of the plate. Explain how this viscous drag can be computed from the given data even though we do not know the fluid viscosity.
Solve Problem 9.13 with the velocity profile at section bc given by the parabolic expression from Problem 9.8. 9.13 A fluid, with density ρ = 1.5 slug/ft 3 , flows at U = 10 ft/s over a flat plate 10 ft long and 3 ft wide. At the trailing edge, the boundary-layer thickness is δ = 1 in. Assume the velocity profile is linear, as shown, and that the flow is two-dimensional (flow conditions are independent of z ). Using control volume abcd , shown by the dashed lines, compute the mass flow rate across surface ab . Determine the drag force on the upper surface of the plate. Explain how this viscous drag can be computed from the given data even though we do not know the fluid viscosity.
Solve Problem 9.13 with the velocity profile at section bc given by the parabolic expression from Problem 9.8.
9.13 A fluid, with density ρ = 1.5 slug/ft3, flows at U = 10 ft/s over a flat plate 10 ft long and 3 ft wide. At the trailing edge, the boundary-layer thickness is δ = 1 in. Assume the velocity profile is linear, as shown, and that the flow is two-dimensional (flow conditions are independent of z). Using control volume abcd, shown by the dashed lines, compute the mass flow rate across surface ab. Determine the drag force on the upper surface of the plate. Explain how this viscous drag can be computed from the given data even though we do not know the fluid viscosity.
13.38 Consider the attic of a home located in a hot climate.
The floor of the attic is characterized by a width of
L₁ = 8 m while the roof makes an angle of 0 = 30° from
the horizontal direction, as shown in the schematic.
The homeowner wishes to reduce the heat load to the
home by adhering bright aluminum foil (ε = 0.07) onto
the surfaces of the attic space. Prior to installation of
the foil, the surfaces are of emissivity & = 0.90.
Attic
A2, 82, T2 0 = 30°
A1, E1, T₁
土
L₁ = 8 m
(a) Consider installation on the bottom of the attic
roof only. Determine the ratio of the radiation heat
transfer after to before the installation of the foil.
(b) Determine the ratio of the radiation heat transfer
after to before installation if the foil is installed
only on the top of the attic floor.
(c) Determine the ratio of the radiation heat transfer if
the foil is installed on both the roof bottom and the
floor top.
13.1
Determine F2 and F2 for the following configura-
tions using the reciprocity theorem and other basic
shape factor relations. Do not use tables or charts.
(a) Small sphere of area A, under a concentric hemi-
sphere of area A₂ = 3A₁
A₂
A1
(a)
(b) Long duct. Also, what is F₁₂?
A₂
Αν
(b)
(c) Long inclined plates (point B is directly above the
center of A₁)
B
100 mm
A₂
- 220 mm
(c)
(d) Long cylinder lying on infinite plane
+
A₁
Az
(d)
(e) Hemisphere-disk arrangement
-A₂, hemisphere,
diameter D
A₂
A₁, disk,
diameter D/2
(e)
(f) Long, open channel
1 m
AA₂
2 m
(f)
(g) Long cylinders with A₁ = 4A₁. Also, what is F₁₂?
-D₁
A1
-A₂
-D2
(e)
(h) Long, square rod in a long cylinder. Also, what
is F22?
w=D/5
18
A₁
-A2
(h)
-D
Chapter 9 Solutions
Fox And Mcdonald's Introduction To Fluid Mechanics
Degarmo's Materials And Processes In Manufacturing
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