ME421Lec3
Transcript of ME421Lec3
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ME421
HeatExchanger andSteamGenerator Design
Lecture 3
Heat Transfer Correlations
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Task
• We need to find average heat transfer coefficient (h) touse in U calculation in place of hi or ho. (Q = UAF∆ Tlm)
• Average Nusselt number (Nu=hL/k) can be obtained from
an appropriate correlation, with general formNu = f(Re, Pr)
• Chapter 3 of our textbook deals with forced convection
correlations for single phase flow only.• Chapters 6-8 of Incropera & DeWitt are good references
as well.
• Both sides or only one side of a heat exchanger may besingle phase, the correlations here are for the singlephase side(s).
• We will cover phase change in Chapter 7 of our textbook.
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Correlations
• Most of the correlations are empirical (obtained fromexperimental results)
• For the sake of generality they are given in terms of non-dimensional groups (Re, Pr, Nu etc.)
• They are only valid for the given conditions or ranges of variables. (Re range, temperatures for propertyevaluation, etc.)
• Check for the ranges and conditions and select the rightcorrelation.
• We need to determine some properties and plug theminto the correlation. These properties are generally eitherevaluated at mean (bulk) fluid temperature or at wall
temperature. Each correlation should also specify this.
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Selecting the right correlation
• Calculate Re and check the flow regime (laminar orturbulent)
• Calculate hydrodynamic entrance length (xfd,h or Lhe) tosee whether the flow is hydrodynamically fullydeveloped. (fully developed flow vs. developing)
• Calculate thermal entrance length (xfd,t
or Lte) to
determine whether the flow is thermally fully developed
• A heat transfer problem may involve combinations of hydrodynamic and thermal development; design
correlations must be selected accordingly.
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Dimensionless Groups
• Re=UL/ν where U and L are characteristic velocity andlength, and ν is kinematic viscosity.
(ratio of inertial to viscous forces)
• Pr=ν/α where α is thermal diffusivity.
(ratio of momentum and thermal diffusivities)
• Local Nux=hxL/k where hx is the local heat transfercoefficient and k is thermal conductivity of fluid.
(dimensionless temperature gradient)
• Mean Nu=hL/k is average Nu over a given length.
• Peb=PrbRe is Pecletnumber based on bulk fluidproperties.
(dimensionless independent heat transfer parameter)
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Characteristic length
• In case of internal flow: L=Dh hydraulic diameter or L=De
equivalent diameter
• Dh=4Ac/Pw where Ac is cross sectional area and Pw iswetted perimeter
• De=4A
c/P
hwhere P
his heated perimeter.
• For hydrodynamical considerations use Dh (Re, etc.)
• For thermal considerations use De (Nu, etc.)
• Circular tube => L=D (diameter of the tube)
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Characteristic velocity
• For internal flow, characteristic velocity is the mean fluidvelocity um.
• Related to mean fluid velocity
– Mass flow rate:
– Mass velocity:
Note that usually mass flow rate is known.
m cm u A ρ =&
mG u ρ =
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Concentric annular duct• Concentric annular ducts are quite common in heat
exchanger designs (e.g. double pipe heat exchanger)
• Ac=π(Di
2
-do
2
)/4, Pw=π(Di+do), Ph=πdo• Dh=(Di
2-do2)/(Di+do)=Di-do
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Variable properties
• Wall temperature Ts or Tw
• Fluid temperature Tb (fluid mean bulk temperature)
• For small changes Ti or To may also be used
• For example there may be a large radial temperaturegradient in circular duct. At what temperature properties are
evaluated matters.
• There may be a need for temperature correction incorrelations.
• Indices cp and vp correspond to constant and variableproperties.
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• Some properties are strong functions of temperature.
Convention for correction:– For liquids lump all property variations to µ (dynamic
viscosity). Sometimes variations are lumped to Pr.
– For gases use temperature dependence directly(everything depends on T)
• Fluids:
• Gases:
where n and m depends on the case.
,
n m
b b
cp w cp w
Nu f Nu f
µ µ
µ µ ⎛ ⎞ ⎛ ⎞= =⎜ ⎟ ⎜ ⎟⎝ ⎠ ⎝ ⎠
,
n m
w w
cp b cp b
T TNu f Nu T f T
⎛ ⎞ ⎛ ⎞= =⎜ ⎟ ⎜ ⎟⎝ ⎠ ⎝ ⎠
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Correlations in the textbook
• Tables 3.1-3.5 are for circular ducts, both laminar andturbulent flow
• Tables 3.6 and 3.7 are correlations specificallydeveloped for variable properties.
• Table 3.8 shows laminar flow correlations for ducts of various cross sections
• For turbulent flow, Tables 3.3, 3.4, 3.6, 3.7 can also beused for noncircular ducts by considering Dh
• Section 3.8 deals with tube bundles (in External Flow
chapter of Incropera & DeWitt, it is a bit better)• Section 3.9 is for helical coils and spirals
• Section 3.10 is for bends (for example U bend in U tube
shell-and-tube heat exchanger)
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Tables in the textbook
• Table 3.1: Laminar forced convection correlations insmooth straight circular ducts
• Table 3.2: Exponents n and m for variable physical
properties associated with Eqns. (3.21) and (3.22) forlaminar forced convection through circular ducts
• Table 3.3: Turbulent forced convection correlations
through a circular duct with constant properties• Table 3.4: Turbulent flow isothermal Fanning friction
factor correlations for smooth circular ducts
• Table 3.5: Exponentsn
andm
for variable physicalproperties associated with Eqns. (3.21) and (3.22) forturbulent forced convection through circular ducts
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Tables in the textbook (continued)
• Table 3.6: Turbulent forced convection correlations incircular ducts for liquids with variable properties
• Table 3.7: Turbulent forced convection correlations in
circular ducts for gases with variable properties• Table 3.8: Nu and f for hydrodynamically and thermally
developed laminar flow in ducts of various cross sections
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Table 3.3
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Table 3.4
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Which correlation is better?
• Usually newer correlations are more accurate thanolder ones.
• More general ones are less accurate compared to
more specific ones.• Usually textbook correlations are as general as
possible. Search journal databases for morespecialized geometries/materials/fluids etc.
• You can obtain a first approximation using a generalcorrelation then search for more specific ones forbetter accuracy.
• Cited reference search may lead to newercorrelations (Scopus, Web of Science, etc.)• Study the examples in the book.
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Problem 3.1
A fluid flows steadily with a velocity of 6 m/s through acommercial iron rectangular duct whose sides are 1 in. by 2 in.and the length of the duct is 6 m. The average temperature of the fluid is 60oC. The fluid completely fills the duct. Calculatethe surface heat transfer coefficient if the fluid is
(a) Water;
(b) Air at atmospheric pressure;(c) Engine oil (ρ=864 kg/m3, cp=2047 J /kgK, υ=0.0839×10-3
m2/s, Pr=1050, k=0.140 W/mK).