This document discusses convection heat transfer. It begins by defining convection and Newton's Law of Cooling. It then describes the two types of convection: forced convection, which is driven by external forces, and natural (or free) convection, which is driven by buoyancy forces. It also discusses boundary layers, turbulent versus laminar flow, the Reynolds, Nusselt, and Prandtl numbers, and their relationships to convection. Specific examples covered include temperature profiles in pipes, flow over flat plates and cylinders, and forced convection in laminar and turbulent pipe flow.
1. Introduction to Kinematics
2. Methods of Describing Fluid Motion
a). Lagrangian Method
b). Eulerian Method
3. Flow Patterns
- Stream Line
- Path Line
- Streak Line
- Streak Tube
4. Classification of Fluid Flow
a). Steady and Unsteady Flow
b). Uniform and Non-Uniform Flow
c). Laminar and Turbulent Flow
d). Rotational and Irrotational Flow
e). Compressible and Incompressible Flow
f). Ideal and Real Flow
g). One, Two and Three Dimensional Flow
5. Rate of Flow (Discharge) and Continuity Equation
6. Continuity Equation in Three Dimensions
7. Velocity and Acceleration
8. Stream and Velocity Potential Functions
1. Introduction to Kinematics
2. Methods of Describing Fluid Motion
a). Lagrangian Method
b). Eulerian Method
3. Flow Patterns
- Stream Line
- Path Line
- Streak Line
- Streak Tube
4. Classification of Fluid Flow
a). Steady and Unsteady Flow
b). Uniform and Non-Uniform Flow
c). Laminar and Turbulent Flow
d). Rotational and Irrotational Flow
e). Compressible and Incompressible Flow
f). Ideal and Real Flow
g). One, Two and Three Dimensional Flow
5. Rate of Flow (Discharge) and Continuity Equation
6. Continuity Equation in Three Dimensions
7. Velocity and Acceleration
8. Stream and Velocity Potential Functions
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Understand the physical mechanism of convection and its classification.
Visualize the development of velocity and thermal boundary layers during flow over surfaces.
Gain a working knowledge of the dimensionless Reynolds, Prandtl, and Nusselt numbers.
Distinguish between laminar and turbulent flows, and gain an understanding of the mechanisms of momentum and heat transfer in turbulent flow.
Derive the differential equations that govern convection on the basis of mass, momentum, and energy balances, and solve these equations for some simple cases such as laminar flow over a flat plate.
Non dimensionalize the convection equations and obtain the functional forms of friction and heat transfer coefficients.
Use analogies between momentum and heat transfer, and determine heat transfer coefficient from knowledge of friction coefficient.
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Introduction to convection
The dimensionless number and its physical significance
Similarity parameters from the differential equation
Dimensional analysis approach and its application
Numerical on Dimensional analysis approach
Review of Navier-Stokes equation
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2. Topics
Basic concept
Types of convection
Boundary layer
Turbulent flow
Laminar flow
Reynolds number
Nusselt number
Prandl number
3. What is Convection?
Convection is a mode of heat transfer between a solid (or liquid)
surface and its adjacent liquid or gas that is in bulk motion. It
involves combined effect of conduction and fluid motion.
Newton’s Law of Cooling
4. Types of Convection
1. Forced Convection:
- when the fluid is forced to flow over the surface by external means
such as a fan, pump or wind.
1. Natural (or Free) Convection:
- when fluid flow is caused by buoyancy forces that are induced by
density differences due to variation of temperature of the fluid.
6. Dimensional analysis
Dimension analysis can be used to:
Derive an equation .
Check whether an equation is dimensionally correct.
However, dimensionally correct doesn’t necessarily mean
the equation is correct
Find out dimension or units of derived quantities.
7. There are physical quantities which
are dimensionless:
Numerical value
Ratio between the same quantity
angle
Some of the known constants like ln
, log etc.
8. Turbulent And laminar flow
Laminar flow:
Where the fluid moves slowly in layers in a pipe,
without much
mixing among the layers.
Turbulent flow
Opposite of laminar, where considerable mixing
occurs,
velocities are high.
9. Reynolds Number:
The Reynolds number is defined as the ratio of inertial forces
to viscous forces and consequently quantifies the relative importance
of these two types of forces for given flow conditions .
They are also used to characterize different flow regimes within a similar fluid, such
as laminar or turbulent flow:
laminar flow occurs at low Reynolds numbers, where viscous forces are dominant,
and is characterized by smooth, constant fluid motion;
turbulent flow occurs at high Reynolds numbers and is dominated by inertial forces,
which tend to produce eddies, vortices and other flow instabilities.
where:
is the mean velocity of the object relative to the fluid (SI units: m/s)
is a characteristic linear dimension, (travelled length of the fluid; hydraulic
diameter when dealing with river systems) (m)
is the dynamic viscosity of the fluid (Pa·s or N·s/m² or kg/(m·s))
is the kinematics viscosity ( ) (m²/s)
is the density of the fluid (kg/m³).
10. Nusselt Number:
In heat transfer at a boundary (surface) within a fluid, the Nusselt
number (Nu) is the ratio of convective to conductive heat transfer
across (normal to) the boundary.
A Nusselt number close to one, namely convection and conduction of
similar magnitude, is characteristic of "slug flow" or laminar flow. A
larger Nusselt number corresponds to more active convection,
with turbulent flow typically in the 100–1000 range.
11. Prandtl Number
The Prandtl number is a dimensionless number, named after the German
physicist Ludwig Prandtl, defined as the ratio of momentum diffusivity (kinematics
viscosity) to thermal diffusivity. That is, the Prandtl number is given as:
: kinematics viscosity, , (SI units : m2/s)
: thermal diffusivity, , (SI units : m2/s)
: dynamic viscosity, (SI units : Pa s = N s/m2)
: thermal conductivity, (SI units : W/(m K) )
: specific heat, (SI units : J/(kg K) )
: density, (SI units : kg/m3 )
Pr<1 means thermal diffusivity dominates., Pr>1momentum diffusivity dominates
12. Dependence Of transition and
laminar flow
The transition from laminar to
turbulent flow depends on the
surface geometry, surface
roughness, upstream velocity,
surface temperature, and the type
of fluid, among other things, and is
best characterized by the Reynolds
number
13. Laminar and Turbulent Flow In Tubes
Flow in a tube can be laminar or turbulent, depending
on the flow conditions.
Fluid flow is streamlined and thus laminar at low
velocities, but turns turbulent as the velocity is
increased beyond a critical value.
Transition from laminar to turbulent flow does not
occur suddenly; rather, it occurs over some range of
velocity where the flow fluctuates between laminar and
turbulent flows before it becomes fully turbulent.
Most pipe flows encountered in practice are turbulent.
Laminar flow is encountered when highly viscous fluids
such as oils flow in small diameter tubes or narrow
passages.
15. Now consider a fluid at a uniform temperature entering a circular tube
whose surface is maintained at a different temperature. This time, the fluid
particles in the layer in contact with the surface of the tube will assume the
surface temperature. This will initiate convection heat transfer in the tube
and
the development of a thermal boundary layer along the tube. The thickness
of
this boundary layer also increases in the flow direction until the boundary
layer reaches the tube center and thus fills the entire tube, as shown in
Figure
17. PARALLEL FLOW OVER FLAT
PLATES
Consider the parallel flow of a fluid over a flat plate of length L in
the
flow direction, as shown in Fig. 7–6. The x-coordinate is measured
along
the plate surface from the leading edge in the direction of the
flow. The fluid
approaches the plate in the x-direction with a uniform velocity V
and temperature T`.
The flow in the velocity boundary layers starts out as laminar,
but if the plate is sufficiently long, the flow becomes turbulent at
a distance
xcr from the leading edge where the Reynolds number reaches its
critical
value for transition.
The transition from laminar to turbulent flow depends on the
surface geometry,
surface roughness, upstream velocity, surface temperature, and
the type of
fluid, among other things, and is best characterized by the
Reynolds number.
24. Turbulent flow over cylinders
Characteristic length Lc=diameter of the cylinder D
The co-relation used is: Nu=hD/k=C(Re)^n (Pr)^0.33
The constants C and n depends upon flow Reynolds
number.
Further,all properties are evaluated at mean film
temperature.
25. Turbulent flow over spheres
Characteristic length Lc=diameter D of sphere
For flow of gases over sphere Nu=0.37(Re)^0.6
For 25<Re<10^5
For flow of liquids over sphere
Nu=[0.97+0.68(Re)^0.5](Pr)^0.33 for 1<Re<2000
Generalized equation for flow over sphere can also be given as
Nu=2+[0.4(Re)^0.5+0.06(Re)^0.67] (Pr)^0.4(µ/µs)^0.25
Where µs=dynamic viscosity