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Boundary Layer and separation
gradient
pressure
favorable
,
0



x
P
gradient
no
,
0



x
P
0, adverse
pressure gradient
P
x



Flow accelerates Flow decelerates
Constant flow
Flow reversal
free shear layer
highly unstable
Separation point
Flow Separation
Separation
Boundary layer
Wake
Stagnation point
q
2
1/ 2
P P
Cp
U





Inviscid curve
2
1 4sin
Cp q
 
Turbulent
Laminar
q
1.0
0
-1.0
-2.0
-3.0
Drag Coefficient: CD
Supercritical flow
turbulent B.L.
Stokes’ Flow, Re<1
Relatively constant CD
Local Heat Transfer Distribution
q
qq”=h(q)(Ts-T),
Nuq=h(q)D/kf
Local Nusselt number
for airflow normal to a
circular cylinder.
(figure 10-22 from the ITHT text)
Stagnation point
Laminar B.L. growth separation
Laminar to turbulent
transition
Turbulent B.L.
growth
Turbulent separation
Averaged Nusselt Number Correlations of
Cylinders in Cross Flows
Note 1: averaged Nusselt number correlations for the circular cylinder flows
can be found in chapter 10-5. Correlations for other noncircular cylinders in
cross flow can also be found in this chapter (see Table 10-3).
Note 2: Heat transfer between a tube bank (tube bundle) and cross flow is given
in many HT textbooks (for example: see chapter 7 of “Introduction to Heat
Transfer” by Incropera & DeWitt. The configuration is important for many
practical applications, for example, the multiple pass heat exchanger in a
condenser unit. The use of tube bank can not only save the operating space but
also can enhance heat transfer. The wake flows behind each row of tubes are
highly turbulent and can greatly enhance the convective heat transfer. In
general, one can find an averaged convection coefficient using empirical
correlation.
Note 3: Because of its compactness, pressure drop across a tube bank can be
also significant and warrants careful design consideration.
Example
A hot-wire anemometer is a flow device used to measure flow velocity based
on the principle of convective heat transfer. Electric current is passing through
a thin cylindrical wire to heat it up to a high temperature, that is why it is called
“hot-wire”. Heat is dissipated to the fluid flowing the wire by convection heat
transfer such that the wire can be maintained at a constant temperature.
Determine the velocity of the airstream (it is known to be higher than 40 m/s
and has a temperature of 25°C), if a wire of 0.02 mm diameter achieved a
constant temperature of 150°C while dissipating 50 W per meter of electric
energy.
Hot-wire, 0.02 mm dia.
Constant temperature 150°C
25°C, U>40 m/s
Air (87.5°C), Pr=0.707, n=1510-6
m2/s, k=0.026 W/m.K
Example (cont.)
2
3
6
0.466 1/3
( )
50 ( )(150 25)
50
6369( / . )
(0.02 10 )(1)(125)
6369(0.00002)
4.90
0.026
VD (40)(0.00002)
Re > 53,
15 10
assume 4000 > Re > 40, use equation (10-37)
(0.683) Re Pr
4.90 (0
S
q hA T T
h DL
h W m K
hD
Nu
k
Nu


n



 
 
 

  
 


  
0.466
1/3
.683) (0.707)
65.9( / ), Re 87.9 satisfy the range of validity
VD
V m s
n
 

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boundary layer & separation.ppt

  • 1. Boundary Layer and separation gradient pressure favorable , 0    x P gradient no , 0    x P 0, adverse pressure gradient P x    Flow accelerates Flow decelerates Constant flow Flow reversal free shear layer highly unstable Separation point
  • 2. Flow Separation Separation Boundary layer Wake Stagnation point q 2 1/ 2 P P Cp U      Inviscid curve 2 1 4sin Cp q   Turbulent Laminar q 1.0 0 -1.0 -2.0 -3.0
  • 3. Drag Coefficient: CD Supercritical flow turbulent B.L. Stokes’ Flow, Re<1 Relatively constant CD
  • 4. Local Heat Transfer Distribution q qq”=h(q)(Ts-T), Nuq=h(q)D/kf Local Nusselt number for airflow normal to a circular cylinder. (figure 10-22 from the ITHT text) Stagnation point Laminar B.L. growth separation Laminar to turbulent transition Turbulent B.L. growth Turbulent separation
  • 5. Averaged Nusselt Number Correlations of Cylinders in Cross Flows Note 1: averaged Nusselt number correlations for the circular cylinder flows can be found in chapter 10-5. Correlations for other noncircular cylinders in cross flow can also be found in this chapter (see Table 10-3). Note 2: Heat transfer between a tube bank (tube bundle) and cross flow is given in many HT textbooks (for example: see chapter 7 of “Introduction to Heat Transfer” by Incropera & DeWitt. The configuration is important for many practical applications, for example, the multiple pass heat exchanger in a condenser unit. The use of tube bank can not only save the operating space but also can enhance heat transfer. The wake flows behind each row of tubes are highly turbulent and can greatly enhance the convective heat transfer. In general, one can find an averaged convection coefficient using empirical correlation. Note 3: Because of its compactness, pressure drop across a tube bank can be also significant and warrants careful design consideration.
  • 6. Example A hot-wire anemometer is a flow device used to measure flow velocity based on the principle of convective heat transfer. Electric current is passing through a thin cylindrical wire to heat it up to a high temperature, that is why it is called “hot-wire”. Heat is dissipated to the fluid flowing the wire by convection heat transfer such that the wire can be maintained at a constant temperature. Determine the velocity of the airstream (it is known to be higher than 40 m/s and has a temperature of 25°C), if a wire of 0.02 mm diameter achieved a constant temperature of 150°C while dissipating 50 W per meter of electric energy. Hot-wire, 0.02 mm dia. Constant temperature 150°C 25°C, U>40 m/s Air (87.5°C), Pr=0.707, n=1510-6 m2/s, k=0.026 W/m.K
  • 7. Example (cont.) 2 3 6 0.466 1/3 ( ) 50 ( )(150 25) 50 6369( / . ) (0.02 10 )(1)(125) 6369(0.00002) 4.90 0.026 VD (40)(0.00002) Re > 53, 15 10 assume 4000 > Re > 40, use equation (10-37) (0.683) Re Pr 4.90 (0 S q hA T T h DL h W m K hD Nu k Nu   n                     0.466 1/3 .683) (0.707) 65.9( / ), Re 87.9 satisfy the range of validity VD V m s n  