ANWESA KAR
M.TECH(THERMAL ENGG.)
1.REYNOLDS NUMBER
 It is the ratio of inertia force to the viscous force.
Where,
Re
VL


 is density
is velocity
L is linear dimension
 is viscosity
Significance-It is used to identify the nature of
flow (Laminar or Turbulent)
V
2.FROUDE NUMBER
 It is the ratio of inertia force to the gravity force
 Where ,
V is the velocity
g is the acceleration due to gravity
L is the characteristics length
Significance-It is used to analyze nature of flow where
free surface is present. e.g. weirs ,channels ,spillways
V
Fr
gL

3.WEBERS NUMBER
 It is the ratio of inertia force to surface tension force.
 Where
V is the velocity
L is the characteristics length
Significance-It is used in analyzing formation of droplet
and in capillary studies.
/
V
We
L 

 is the surface tension
 is the density
4.EULER NUMBER
 It is the ratio of inertia force to pressure force.
 Where
P is the pressure
V is the velocity
Significance-It is used to characterize energy losses in a
flow.
V
Eu
P


 is the density
5.MACH NUMBER
 It is the ratio of inertia force to elastic force.
 Where
V is the velocity of object
C is the speed of sound
Significance-It is used to analyze fluid flow where
compressibility is a important factor.
V
M
C

6.BIOT NUMBER
 It is the ratio of conductive resistance to convective
resistance.
Where
h is the heat transfer coefficient
K is the thermal conductivity
Significance-It is used in the heat transfer calculation
(lumped heat analysis).
chL
Bi
K

cL is the characteristics length(volume of
the body/surface area of contact)
7.FOURIER NUMBER
 It is the ratio of heat conducted through a body to the
heat stored.
 Where,
t is the characteristics time
 Significance-It is used in transient heat analysis.
2
c
t
L

 
 is the thermal diffusivity
cL is the length
8.NUSSELT NUMBER
It is the ratio of convective heat transfer to conductive heat
transfer.
Where
h is the convective heat transfer coefficient
L is the characteristics length
K is the thermal conductivity
Significance-It describe the enhancement of heat transfer
because of convection in comparison to conduction
hL
Nu
K

9.PRANDTL NUMBER
 It is the ratio of momentum diffusivity to heat diffusivity
 Where
K is the thermal conductivity
Significance-Prandtl number is used to describe thermal
boundary layer.
Pr PC
K


 is the dynamic viscosity
PC is the specific heat
10.GRASHOF NUMBER
 It is the ratio of buoyancy force to viscous force.
 Where
g is acceleration due to gravity
Significance-It is used in flow analysis in natural convection.
 is the coefficient of thermal expansion
sT is the surface temperature
T is the fluid temperature far from the surface
 is the kinematic viscosity of fluid
3
2
( )s cg T T L
Gr




11.RAYLEIGH NUMBER
 Rayleigh number is the product of Grashof number
and Prandtl number.
Ra= Gr . Pr
Significance-It is associated with buoyancy driven flow .
Its value is used to characterize laminar to turbulent
transition.
12.STANTON NUMBER
 It is defined as the ratio of heat transferred by convection
to the heat capacity of fluid.
 Where h is the heat transfer coefficient
u is the speed of fluid
Significance-It is used in heat transfer for forced
convection flows.
Re.Pr p
Nu h
St
uC
 
 is the density of fluid
pC is the Specific heat capacity of the fluid
13.PECLET NUMBER
 It is defined as the product of Reynold number and
Prandtl number.
 Where
L is the characteristics length
u is the velocity
Significance-It is used in calculations including
convective heat transfer rate.
Re.Pr
Lu
Pe

 
 is the thermal diffusivity
14.JAKOB NUMBER
 It is the ratio of sensible energy absorbed to latent
energy absorbed during liquid- vapor phase change.
 Where
Significance-It is used in analyzing flow pattern in
process of boiling.
( )P s sat
fg
C T T
Ja
h


PC
s satT T
fgh
is the specific heat capacity
is the temperature difference
Latent heat of vaporization
15.BOND NUMBER
 It is the ratio of buoyancy force to the surface tension
force.
 Where
g is the acceleration due to gravity
Significance-It is used in analyzing the behavior of
bubbles.
1 2( )g
Bo
 



1 2( )  is the difference in density
 is the surface tension
16.SCHIMDT NUMBER
 It is the ratio of momentum diffusivity to mass
diffusivity.
 Where
D is the mass diffusivity
Significance-It is used in fluid flows where simultaneous
mass and momentum diffusion occurs.
Sc
D


 is the kinematic viscosity
17.LEWIS NUMBER
 It is the ratio of thermal diffusivity to the mass diffusivity.
Where
D is the mass diffusivity
K is the thermal conductivity
Significance-It is used to analyze fluid flow with
simultaneous heat and mass transfer by convection.
p
K
Le
D C D


 
 is the thermal diffusivity
pC is the specific heat capacity
18.SOMMERFELD NUMBER
 Sommerfeld number is defined by the following equation
Where
r is the radius of the journal
c is the radial clearance
P is the bearing pressure
Significance-It is used in hydrodynamic lubrication
analysis.
2
. snr
S
c P
 
  
 
 is the dynamic viscosity
sn is the journal speed in r.p.s
19.KNUDSEN NUMBER
 It is the ratio of molecular mean free path to the
characteristics length.
 Where
L is the characteristics length
Significance-It is useful in determining whether
continuum mechanics formulation can be applied or
not in a system.
Kn
L


 is the mean free path
20.SHERWOOD NUMBER
 It is the ratio of convection mass transfer to the
diffusion mass transfer
 Where
K is the mass transfer coefficient
l is the characteristics length
D is the mass diffusivity
Significance-It is used in mass transfer problems.
Kl
Sh
D

Dimensionless number

Dimensionless number

  • 1.
  • 2.
    1.REYNOLDS NUMBER  Itis the ratio of inertia force to the viscous force. Where, Re VL    is density is velocity L is linear dimension  is viscosity Significance-It is used to identify the nature of flow (Laminar or Turbulent) V
  • 3.
    2.FROUDE NUMBER  Itis the ratio of inertia force to the gravity force  Where , V is the velocity g is the acceleration due to gravity L is the characteristics length Significance-It is used to analyze nature of flow where free surface is present. e.g. weirs ,channels ,spillways V Fr gL 
  • 4.
    3.WEBERS NUMBER  Itis the ratio of inertia force to surface tension force.  Where V is the velocity L is the characteristics length Significance-It is used in analyzing formation of droplet and in capillary studies. / V We L    is the surface tension  is the density
  • 5.
    4.EULER NUMBER  Itis the ratio of inertia force to pressure force.  Where P is the pressure V is the velocity Significance-It is used to characterize energy losses in a flow. V Eu P    is the density
  • 6.
    5.MACH NUMBER  Itis the ratio of inertia force to elastic force.  Where V is the velocity of object C is the speed of sound Significance-It is used to analyze fluid flow where compressibility is a important factor. V M C 
  • 7.
    6.BIOT NUMBER  Itis the ratio of conductive resistance to convective resistance. Where h is the heat transfer coefficient K is the thermal conductivity Significance-It is used in the heat transfer calculation (lumped heat analysis). chL Bi K  cL is the characteristics length(volume of the body/surface area of contact)
  • 8.
    7.FOURIER NUMBER  Itis the ratio of heat conducted through a body to the heat stored.  Where, t is the characteristics time  Significance-It is used in transient heat analysis. 2 c t L     is the thermal diffusivity cL is the length
  • 9.
    8.NUSSELT NUMBER It isthe ratio of convective heat transfer to conductive heat transfer. Where h is the convective heat transfer coefficient L is the characteristics length K is the thermal conductivity Significance-It describe the enhancement of heat transfer because of convection in comparison to conduction hL Nu K 
  • 10.
    9.PRANDTL NUMBER  Itis the ratio of momentum diffusivity to heat diffusivity  Where K is the thermal conductivity Significance-Prandtl number is used to describe thermal boundary layer. Pr PC K    is the dynamic viscosity PC is the specific heat
  • 11.
    10.GRASHOF NUMBER  Itis the ratio of buoyancy force to viscous force.  Where g is acceleration due to gravity Significance-It is used in flow analysis in natural convection.  is the coefficient of thermal expansion sT is the surface temperature T is the fluid temperature far from the surface  is the kinematic viscosity of fluid 3 2 ( )s cg T T L Gr    
  • 12.
    11.RAYLEIGH NUMBER  Rayleighnumber is the product of Grashof number and Prandtl number. Ra= Gr . Pr Significance-It is associated with buoyancy driven flow . Its value is used to characterize laminar to turbulent transition.
  • 13.
    12.STANTON NUMBER  Itis defined as the ratio of heat transferred by convection to the heat capacity of fluid.  Where h is the heat transfer coefficient u is the speed of fluid Significance-It is used in heat transfer for forced convection flows. Re.Pr p Nu h St uC    is the density of fluid pC is the Specific heat capacity of the fluid
  • 14.
    13.PECLET NUMBER  Itis defined as the product of Reynold number and Prandtl number.  Where L is the characteristics length u is the velocity Significance-It is used in calculations including convective heat transfer rate. Re.Pr Lu Pe     is the thermal diffusivity
  • 15.
    14.JAKOB NUMBER  Itis the ratio of sensible energy absorbed to latent energy absorbed during liquid- vapor phase change.  Where Significance-It is used in analyzing flow pattern in process of boiling. ( )P s sat fg C T T Ja h   PC s satT T fgh is the specific heat capacity is the temperature difference Latent heat of vaporization
  • 16.
    15.BOND NUMBER  Itis the ratio of buoyancy force to the surface tension force.  Where g is the acceleration due to gravity Significance-It is used in analyzing the behavior of bubbles. 1 2( )g Bo      1 2( )  is the difference in density  is the surface tension
  • 17.
    16.SCHIMDT NUMBER  Itis the ratio of momentum diffusivity to mass diffusivity.  Where D is the mass diffusivity Significance-It is used in fluid flows where simultaneous mass and momentum diffusion occurs. Sc D    is the kinematic viscosity
  • 18.
    17.LEWIS NUMBER  Itis the ratio of thermal diffusivity to the mass diffusivity. Where D is the mass diffusivity K is the thermal conductivity Significance-It is used to analyze fluid flow with simultaneous heat and mass transfer by convection. p K Le D C D      is the thermal diffusivity pC is the specific heat capacity
  • 19.
    18.SOMMERFELD NUMBER  Sommerfeldnumber is defined by the following equation Where r is the radius of the journal c is the radial clearance P is the bearing pressure Significance-It is used in hydrodynamic lubrication analysis. 2 . snr S c P         is the dynamic viscosity sn is the journal speed in r.p.s
  • 20.
    19.KNUDSEN NUMBER  Itis the ratio of molecular mean free path to the characteristics length.  Where L is the characteristics length Significance-It is useful in determining whether continuum mechanics formulation can be applied or not in a system. Kn L    is the mean free path
  • 21.
    20.SHERWOOD NUMBER  Itis the ratio of convection mass transfer to the diffusion mass transfer  Where K is the mass transfer coefficient l is the characteristics length D is the mass diffusivity Significance-It is used in mass transfer problems. Kl Sh D 