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Heat Transfer and Fluid Heat Transfer and Fluid Flow Over a Flat PlateFlow Over a Flat Plate
MANE 4020Fall 2005
(x)
U0
U(y)
U
xo
U(x,0)=0
Boundary layer thickness: yU(y)/ U =0.99
Fluid Problem: Friction and Fluid Problem: Friction and Boundary layerBoundary layer
s u
yy0
Shear stress
Measurement of the Velocity ProfileMeasurement of the Velocity Profile
ptotal pstatic1
2 U2
U
Laminar flow
Turbulent flow
Skin Friction CoefficientSkin Friction Coefficient
C f s
12 U
2
C f
2
0.332
Rex1/ 2
C f
2
0.0296
Rex1/ 5
Re x U x
Skin Friction Correlations
Skin Friction Measurement
s u
yy0
From: (difficult to get u near to wall)
Boundary layer modelsBoundary layer models
71
y
U
u
u y
u 1
ln y B
y yu u u u ; u s
y+ 30
y+ 5
1/7th Power Law
More exact expression
Boundary layer modelsBoundary layer models
Convection Heat TransferConvection Heat Transfer
It quantifies the energy transfer between a fluid at one temperature flowing over a solid object at a different temperature.
h q
T
q
AT- q” is the heat flux (J/s m2 = W/m2)T is the difference between fluid temperature (in the freestream) and the solid wall temperature-A is the surface area of the solid. -q is the total heat transfer from a surface (Watts).
Two common questions of any Two common questions of any convective heat transfer problemconvective heat transfer problem
Given the distribution of surface temperature as a function of position along a surface, what is the distribution of local heat flux?
Given the distribution of local surface heat flux as a function of position along a surface, what is the
distribution of surface temperature? Tfluid
Tsolid
Fluid flow and heat transfer over Fluid flow and heat transfer over flat plate - A complex problemflat plate - A complex problem
(x)
U0 , T0
U(x,y) Tw (x)
T (x)U (x)
(x)
T(x,y)
xo qw qw qw qw
U(x,0)=0 Tw>Tinf
Rex= U *x/is the criterion for the Turbulent/LaminarRex>105 for the flat plate flowRed >2300, for the pipe flow
Stx h
cpUfunc
Ux
,
h is the property of flow Pr is the property of fluid
Stx 0.453Re x0.5 Pr 2/ 3
Stx 0.0307Re x0.2 Pr 0.4
Laminar flow – can be derived
Turbulent flow - experimental
Dimensionless heat transfer Dimensionless heat transfer coefficient (Stanton #)coefficient (Stanton #)
St decreases with the increase of Re.St increases when the flow becomes turbulent flow.
Measurement of heat transfer Measurement of heat transfer coefficient (I)coefficient (I)
Q0
QconvectionQradiation
Qconduction
Qo Qconvection Qbackside Qradiation
Tblack
TT
Tplate
Rconv
R rad
Rcond
Measurement of heat transfer Measurement of heat transfer coefficient (II)coefficient (II)
The plate is constructed of four layers of materials:• Four, 2 in. wide Ni-Chrome heating strips which are embedded in
fiberglass and epoxy resin;• 3/8 in. balsa wood;
• 5/8 in. plywood;• 1/8 in. plywood.
Qo Qconvection Qbackside Qradiation
Qo = VI Qconvection
Ts TR conv
hA(Ts T )
Qbackside Ts Tback
Rplate
44surrSradiation TTAQ
Tblack
TT
Tplate
Rconv R rad
Rcond
h
Measurement of heat transfer Measurement of heat transfer coefficient (III)coefficient (III)
Structure of Wind TunnelStructure of Wind Tunnel
Wind supply: Blower /Fan (quantity supply); Settling chamber (quality supply)
Honeycomb, Mesh Screen To reduce turbulence