hydrodynamics and heat transfer in nuclear reactor
TRANSCRIPT
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Hydrodynamics and heat transfer in nuclear reactor
Lecture 7. CONVECTIVE HEAT
TRANSFER IN NUCLEAR REACTOR
Lecturer: prof. Alexander Korotkikh
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Contents
Introduction
Factors influencing the heat transfer
Modeling of process of convective heat transfer
Heat transfer in single-phase fluid with free flow (natural convection)
Heat transfer in single-phase fluid with forced flow (forced convection)
Heat transfer in forced cross flow pipes and bundles of pipes
The heat transfer to liquid metals
Heat transfer to water boiling
Conclusion
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Introduction
Convection heat transfer is always accompanied by thermal conductivity, since the motion of the fluid or gas unavoidably contact the individual particles with different temperatures. In the practical calculations of heat transfer using Newton- Richman law:
( ) , [W]s lQ t t F
Specific conditions are taken into account by the coefficient of proportionality , which call the heat transfer coefficient.
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Factors which influence on the heat transfer
1. The origin of motion (free or forced). Free movement or natural convection occurs under the influence of the density difference of cold and hot fluid particles (gas). Forced movement (forced convection) occurs under the influence of the pressure difference created by a pump, compressor. In some cases, along with forced, at the same time can develop free traffic. The relative influence of the latter the greater the greater the temperature difference in the individual volumes of liquid (gas) and less than the speed of the forced movement.
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Factors which influence on the heat transfer
2. The flow regime (laminar, transition, turbulent). In laminar flow the particles of fluid (gas) are moving quietly, without mixing (Fig. a), the heat transfer from surface to fluid (gas) is thermal conductivity. The turbulent regime is characterized by continuous mixing of all liquid layers (Fig. b). In this case, the wall surface is formed of a laminar sublayer of liquid with thickness ls . The heat transfer from wall surfase to fluid and turbulent flow is performed by conduction and convection. Intermediate regime of fluid motion between laminar and turbulent is called transitional.
a) Laminar b) Turbulent
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Factors which influence on the heat transfer
3. Hydrodynamic and thermal boundary layers. In any mode of motion of particles of fluid immediately adjacent to a solid surface, as would stick to it. As a result close to the streamlined surface under the action of viscous friction forces formed a flat liquid layer near retarded which the fluid velocity changes from zero (at the surface of the body) to the velocity of the undisturbed flow (away from body). This retarded layer of fluid is called hydrodynamic boundary layer. Similarly, the concept of hydrodynamic boundary layer there is the concept of thermal boundary layer. This liquid layer , adjacent to a solid surface, within which the temperature liquid varies from the wall temperature ts to the temperature of the stream away from the surface tl. The ratio of the thickness of thermal and hydrodynamic boundary layers is determined by the value of the Prandtl number Pr = v/a, where v – kinematic viscosity, a - is the thermal diffusivity of liquid.
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Factors which influence on the heat transfer
4. Thermophysical properties of the fluid. The heat transfer coefficient depends on the heat conductivity , heat capacity cp, kinematic viscosity , density , the coefficient of volume expansion and other fluid properties. In particularly, in the presence of phase transitions (boiling, condensation), from heat of evaporation r, surface tension etc. 5. Geometric size, shape, orientation of heat transfer surface. Is established that the heat transfer coefficient depends on the geometrical shape of the body surface (planar, cylindrical, spherical or other), sizes (length of the surface, the diameter of the tube or sphere, etc.), orientation of the heat transfer surface (vertical, horizontal with heat transfer upwards, horizontal with heat transfer down, sloped, etc.).
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Modeling of process of convective heat transfer
the Nusselt number it characterizes the intensity of convective heat exchange, where – thermal conductivity of liquid environment; l is the geometric dimension (length);
Nul
the Reynolds number it characterizes the ratio of forces inertia and forces of viscosity, where w is the velocity of the flow, – kinematic viscosity;
Rewl
the Prandtl number it characterizes the thermophysical properties of the fluid, where a is the thermal diffusivity;
Pra
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Modeling of process of convective heat transfer
the Peclet number here the numerator characterizes the heat carried by convection and the denominator is the heat transported by conduction;
Pe Re Prwl
a
the Grashof number it characterizes the attitude lift force occurs due to the difference of the densities of the liquid due to temperature changes t , to viscous forces, where is the coefficient of volume expansion;
3
2Gr
g t l
The Nusselt number Nu is determined by the number of tasks convective heat transfer, because it contains the sought value of heat transfer coefficient . The other similarity number (Re, Pr, Gr, Pe ...) are crucial and include quantities which depend on the heat transfer coefficient.
Nu = f(Re, Pr, Gr, Pe …).
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Modeling of process of convective heat transfer
When modeling the heat transfer, the experimental results are processed in the similarity and relationship between them are in the form of the similarity equations
Nu Re Pr ,n m
ld ld lC
Nu ,ld
d
Re ,ld
w d
ν
where C, m, n – constant coefficients determined experimentally.
PrNu (Gr Pr ) ,
Pr
m
n llх lх l
s
C
3
2Gr .lх
g t x
where
or
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Heat transfer at free convection of fluid
Heat transfer coefficient
with the free motion of fluid
3 910 Gr Pr 10lx l – laminar regime
– transition regime
– turbulent regime
9 1010 Gr Pr 6 10lx l
10Gr Pr 6 10lx l
3
2Gr ,lх
g t x
Grashof number
s lt t t – the temperature difference
= f(t) are given in manuals for liquids. For gases are calculated 1
.lT
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Heat transfer at free convection of fluid
0.25
0.25 PrNu 0.60(Gr Pr )
Pr
llх lх l
s
Laminar regime
local value of
0.25
0.25 PrNu 0.75(Gr Pr )
Pr
llh lh l
s
average value of lam
Turbulent regime
0.25
1/3 PrNu 0.15(Gr Pr )
Pr
llх lх l
s
local and average value of turb
Transition regime
.2
turb lamtrans
Vertical surface
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Heat transfer at free convection of fluid
For horizontal flat surfaces (plates) the above formula is applicable for calculation, but in this case decrease by 30 %, if the heat transfer surface facing downt. The calculated heat transfer coefficient should be increased by 30 %, if the heat-transfer surface facing upward.
For horizontal pipes with laminar regime of fluid flow to calculate the average heat transfer coefficient
0.25
0.25 PrNu 0.5(Gr Pr )
Pr
lld ld l
s
Horizontal surface
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Heat transfer at forced convection of fluid
The boundary layer and modifying the heat
transfer coefficient along the surface
Horizontal surface
The forced fluid flow (forced convection) occurs under the action of pressure difference, which in conjunction with the thermal properties determines the fluid velocity w.
4Re 10lх – laminar regime 4 610 Re 4 10lх – transition regime
6Re 4 10lх – turbulent regime 0.25
0.5 0.33 PrNu 0.66 Re Pr
Pr
lll ll l
s
0.25
0.8 0.43 PrNu 0.037 Re Pr
Pr
lll ll l
s
– laminar, Re<5·105
– turbulent, Re>5·105
Rell
w l
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Heat transfer at forced convection of fluid
Reld
w d
Re 2300ld
42300 Re 10ld
4Re 10ld
Channel
– laminar regime
– transition regime
– turbulent regime
At laminar flow regime of fluid in pipe distinguish viscous and viscous-gravitational modes.
0.140.33
Nu 1.55 Pe sld ld l
l
d
l
– viscous regime
Pe Re Prw d
a
– the coefficient of dynamic viscosity, d, l – inner diameter and length of the pipe,
5(Gr Pr ) 8 10 ,ld l Re 2300ld
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Heat transfer at forced convection of fluid
5(Gr Pr ) 8 10 ,ld l Re 2300ld Viscous-gravitational regime – 0.25
0.33 0.43 0.1 PrNu 0.15 Re Pr Gr
Pr
lld ld l ld l
s
l/d 1 2 5 10 15 20 30 40
l 1.9 1.7 1.44 1.28 1.18 1.13 1.05 1.02
0.25
0.8 0.43 PrNu 0.021 Re Pr
Pr
lld ld l l
s
Turbulent regime – 4Re 10ld
1 2
2
l ll
t tt
– average temperature
of liquid or gas
Reld 2300 3000 5000 6000 8000 10000
0.40 0.57 0.72 0.81 0.96 1.00 tr
42300 Re 10ld Transition regime –
tr turb tr
turb
4equ
Fd
P
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Heat transfer in forced cross flow pipes and bundles of pipes
а)
b)
с)
Forced cross flow pipes
Rewd
Re < 40 40 < Re < 1000 Re > 105
= (80 90) = (120 140)
is the separation angle
The character of changes of heat transfer coefficient on the regime of fluid flow
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Heat transfer in forced cross flow pipes and bundles of pipes
0.25
0.4 0.37 PrNu 0.76Re Pr
Pr
lld ld l
s
Re < 40
40 < Re < 1000 0.25
0.5 0.38 PrNu 0.5Re Pr
Pr
lld ld l
s
103 < Re < 2105 0.25
0.6 0.38 PrNu 0.25Re Pr
Pr
lld ld l
s
2105 < Re < 107
0.25
0.8 0.37 PrNu 0.023Re Pr
Pr
lld ld l
s
If the angle of attack < 90 , it was found according to the formulas the heat transfer coefficient should be multiplied by a correction factor
21 0.54cos
To calculate the average heat transfer coefficient around the perimeter of the pipe
average value of
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Heat transfer in forced cross flow pipes and bundles of pipes
0.25
0.5 0.36 PrNu 0.52Re Pr
Pr
lld ld l
s
40 < Re < 103
103 < Re < 105 0.25
0.65 0.33 PrNu 0.26Re Pr
Pr
lld ld l s
s
0.15
2s
s
d
is the correction coefficient taking into account the density the location of the pipes in the beam
Re > 105 0.25
0.84 0.36 PrNu 0.021Re Pr
Pr
lld ld l
s
average value of 3
The first row corridor beam 1 30.6
The second row corridor beam 2 30.9
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Heat transfer in forced cross flow pipes and bundles of pipes
0.25
0.5 0.36 PrNu 0.71Re Pr
Pr
lld ld l
s
40 < Re < 103
103 < Re < 105 0.25
0.60 0.33 PrNu 0.41Re Pr
Pr
lld ld l s
s
is the correction coefficient taking into account the density the location of the pipes in the beam
Re > 105 0.25
0.84 0.36 PrNu 0.021Re Pr
Pr
lld ld l
s
average value of 3
The first row corridor beam 1 30.6
The second row corridor beam 2 30.7
1/6
1
2
s
s
s
sin If the angle of attack < 90
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Heat transfer in forced cross flow pipes and bundles of pipes
, [W]bund l sQ t t F
Convective heat flux
where
1
1
n
i i
ibund n
i
i
F
F
1 2 3( 2)bund
n
n
or
For axial flow bundles of tubes which are cooled by gases or fluids, the average Nusselt number is calculated
0.1 0.4Nu Nu Re Pr 1 2expeq
eqld tur ld l B
0.25
0.8 0.37 PrNu 0.023Re Pr
Pr
ltur ld l
s
where /eqB d d
2
1.1 1s
Bd
2
1.27 1s
Bd
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The heat transfer to liquid metals
Liquid metals are applied in those cases when it is necessary to ensure intensive heat removal from the heating surface or when low pressure is required to have a high temperature working fluid.
Liquid metals have a high boiling point that allows to raise their temperature without applying high pressure.
Pr 0.005 0.05 The Prandtl number
In laminar flow the heat is transferred by the thermal conductivity. In the turbulent is thermal conductivity and convection.
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The heat transfer to liquid metals
When ts=const the values of the Nusselt number from the Peclet number at the laminar regime the flow of liquid metal
1 10 100 1000 104
4.04 3.86 3.74 3.68 3.66
2Peld
Nuld
When q = const the number Nu in the field of stable laminar flow is independent of the number Pe and equal to a constant value:
Nu 4.36ld
0.8Nu 5 0.025Peld ld
When ts=const and the turbulent regime the flow of liquid metal
When q = const 0.8Nu 7 0.025Peld ld