CONVECTIVE CONVECTIVE
HEAT TRANSFER HEAT TRANSFER
By: Prof K. M. Joshi,By: Prof K. M. Joshi,AssiAssi. Professor, MED,. Professor, MED,
SSAS Institute of Technology, Surat.SSAS Institute of Technology, Surat.
MECHANISM BEHIND FREE /NATURAL CONVECTION
The stagnate layer of fluid in
immediate vicinity of hot body
receives heat energy by
conduction. The energy transfer by
this, increases temperature and
internal energy of fluid particles.
Warmer air
rising
AIR.
Q
Because of temperature rise particles become less dance and hence lighter.
The lighter particles move upward in low temperature region.
These particles mix with the cool particles and transfer a part of energy.
Simultaneously cool heavier particles moves downward to fill the space
vacated by warm particles
The circulation pattern, upward movement of hot particles and downward
movement of cool particles causes convective currents. The se currents are
set up naturally due to gravitational force only.
MECHANISM BEHIND FORCED CONVECTION
AIR
20°C
5 m/s
20°C.
Q
Fluid flow causing by the pump, fan or atmospheric wind…
Therefore the rate of heat transfer is much higher by forced convection
than it is by the natural convection or by conduction.
In fact, the higher the fluid velocity, the higher the rate of heat transfer.
EXAMPLES OF NATURAL AND FORCED CONVECTION
�Design of house heating, furnace, architectural
projects, roads and concrete structures concerns with the
free convection.
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�Cooling in IC engines, air condition installations,
temperature control in nuclear plant, condenser tubes or
other heat exchangers are example of forced convection.
Convection heat transfer strongly depends on ….
� fluid properties dynamic viscosity , thermal conductivity k, density
and specific heat
� fluid velocity V
� Geometry and the roughness of the solid surface
� Type of fluid flow (such as being laminar or turbulent).
(((( ))))conv s sQ hA T T∞∞∞∞= −= −= −= −&&&&NEWTON’S LAW OF COOLING
(((( ))))conv s s ∞∞∞∞h = Convection heat transfer coefficient
As = Heat transfer surface area
Ts = Temperature of the surface
T∞∞∞∞= Temperature of the fluid sufficiently far from the surface
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Heat flux, qconv =
The value of convective heat transfer coefficient (as well as
temp difference may also) is not constant for entire surface it
depends on location there for we can define
Local and total convection transfer (a) Surface of arbitrary shape. (b) Flat plate.
LOCAL HEAT FLUX convq′′
(((( ))))conv l sq h T T∞∞∞∞′′′′′′′′ = −= −= −= −
hl is the local convection coefficient
Local and total convection transfer (a) Surface of arbitrary shape. (b) Flat plate.
dAsq”
As, Ts
V ,T∞∞∞∞
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q”
x dxL
As, Ts
U ,T∞ ∞∞ ∞∞ ∞∞ ∞
TOTAL HEAT TRANSFER RATE
s
conv conv s
A
Q q dA′′= ∫&
( )s
conv s l s
A
Q T T h dA∞= − ∫&
convQ&
(((( ))))conv l sq h T T∞∞∞∞′′′′′′′′ = −= −= −= −
putting value of Q&
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1
s
l ss A
h h dAA
= ∫
putting value of convQ&
( )s
conv s l s
A
Q T T h dA∞= − ∫&(((( ))))conv s sQ hA T T∞∞∞∞= −= −= −= −&&&&
An implication of the no-slip and the no-temperature jump
conditions is that heat transfer from the solid surface to the
fluid layer adjacent to the surface is by pure conduction, since
the fluid layer is motionless,
0conv cond fluid
y
Tq q k
dy =
∂= = −& &
T represents the temperature distribution in the fluid
is the temperature gradient at the surface.
( ) 0yT y =∂ ∂is the temperature gradient at the surface.
( )conv l sq h T T∞′′ = −
(((( ))))fluid ys
k T yh
T T====
∞∞∞∞
− ∂ ∂− ∂ ∂− ∂ ∂− ∂ ∂====
−−−−0
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A fluid flowing over a stationary surface comes to a complete stop
at the surface because of the no-slip condition.
Zero velocity
at the surface
Relative velocity
of fluid layersUniform
approach
velocity, V
Solid Block
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A similar phenomenon occurs for the temperature. When two bodies at
different temperatures are brought into contact, heat transfer occurs until
both bodies assume the same temperature at the point of contact.
Therefore, a fluid and a solid surface will have the same temperature at the
point of contact. This is known as NO-TEMPERATURE-JUMP CONDITION.
A steam pipe is passed through a room in which air and walltemperature are al 30 oC while surface temperature of the pipe is400 oC If the diameter of the pipe is 40 mm and average heattransfer coefficient is 20 W/m2 oC, what is the rate of heat lossfrom the pipe for one meter length of pipe.
Schematic:
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Known: surface temperature and air temp
Find: The rate of heat loss
Assumptions: �Steady operating conditions exist. �Radiation effects are negligible. �Constant properties.
Analysis:
Q = h X A X (Ts - Tα)
= 20 X (πdL) X (400 - 30)
= (20 W/m2 oC ) X ( π X 40 X 10 3 X 1 m2 ) X ( 370 oC )
= 0.93 kW
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Laminar versus Turbulent FlowSome flows are smooth and orderly while others are rather chaotic. The
highly ordered fluid motion characterized by smooth streamlines is called laminar.
The flow of high-viscosity fluids such as oils at low velocities is typically laminar.
The highly disordered fluid motion that typically occurs at high velocities
characterized by velocities fluctuations is called turbulent. The flow of low-
viscosity fluids such as air at high velocities is typically turbulent. This flow greatly
influences the heat transfer rates and the required power for pumping
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Smooth well rounded
Entrance
Q = VA
Pipe
Dye
Transitional
Turbulent
Laminar
The Reynolds number can
be viewed as the ratio of
the inertia forces to viscous
forces acting on a fluid
volume element.
Osborne Reynolds
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Dimensionless numbers and
their Physical significance.
Reynolds NumberReynolds NumberReynolds NumberReynolds Number
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Leads to turbulent flowLeads to turbulent flowLeads to turbulent flowLeads to turbulent flow
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WILHEM NUSSELT
(1882-1957)
was a German engineer. Nusselt studied mechanical
engineering at the Munich Technical University where
he got his doctorate in 1907.
�Doctoral thesis – CONDUCTIVITY OF INSULATING MATERIALS
�Professor at Technical university of Karlsruhe - 1920 -1925
�Professor at Technical university of Munchen - 1926 -1952
�Worked till the age of 70 years. Lived for 75 years and died in Munchen on
September 1, 1957.
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CHARACTERISTIC LENGTH OR EQUIVALENT DIAMETERIn the non-dimensional number expressions there has appeared a characteristic length L or diameter De. The equivalent diameter is usually defined as:
For simple tube having internal diameter D,
Ludwig Prandtl
1875-1953
Professor of Applied
Mechanics at Gottingen
for forty-nine years (from
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Mechanics at Gottingen
for forty-nine years (from
1904 until his death
there on August 15,
1953)
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2
32 )(
µβρ Tgl
Gr∆=
Grashof NumberGrashof NumberGrashof NumberGrashof Number
22
2232
)(
)()(
Vl
lVTgl
µρβρ ×∆= 2)(
)()(
forceviscous
forceinertiaforcebuoyant ×=
The Grashof number represents the product of bouyant force and inertia force to the square of viscous force.
The natrual convection start with very small value of Gr and increase with significant increses in Gr.
The role of Grashof number in natural convection is similar to the Reynold number in forced convection.
Gr provides criteria whether the flow is laminar or turbulent.
The critical Gr is 109 for a flow over a vertical plate for change over from laminar to turbulent. ww
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Stanton NumberStanton NumberStanton NumberStanton Number
K
KJ
KKg
KJ
s
m
m
Kg⇒
⋅××
3
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PecletPecletPecletPeclet NumberNumberNumberNumber
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GraetzGraetzGraetzGraetz NumberNumberNumberNumber
Heat capacity of Fluid Heat capacity of Fluid Heat capacity of Fluid Heat capacity of Fluid (in pipe) Per unit Length(in pipe) Per unit Length(in pipe) Per unit Length(in pipe) Per unit Length
Thermal conductivity of Thermal conductivity of Thermal conductivity of Thermal conductivity of pipepipepipepipe
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