1
King Abdulaiz University Faculty of Engineering
Mechanical Engineering Department
MEP460 Heat Exchanger Design
Sep. 2018
LMTD and Effectiveness-NTU Heat exchanger methods
1-Basic types of heat exchangers 2-LMTD method
3-Effectivness-NTU method 4-Compcat heat exchangers 5-Examples
Ch. 11 Incropera (Heat Exchangers)
1-Basic types of heat exchangers
Classification according to flow arrangements Parallel flow arrangement
Counter flow arrangement Cross flow heat arrangement
Counter flow arrangement Parallel flow arrangement
Cross flow heat arrangement
Both fluids are Unmixed cross flow HX with fins
Mixed unmixed heat exchanger with no fins
Classification of heat exchangers according to flow phase
Liquid to liquid HX Liquid to Gas HX Gas to Gas HX
Example Cooling of oil using sea water Using exhaust gases to heat water
(Car radiator)
Heating of air using exhaust gases
Other very common types of heat exchangers
a) Shell and tube heat exchangers b) Compact heat exchangers
Plate-fin compact heat exchanger Tube-fin compact heat exchanger c) Plate heat exchangers
d) Cooling towers
a) Shell and tube heat exchangers
One shell pass and two tube passes Two shell passes and 4 tube passes
b) Compact heat exchangers
Surface area density= 𝛼 A/V [m2/m3]
For compact heat
exchangers 𝛼
> 700𝑚2
𝑚3
c) Plate and frame (Gasketed) heat exchangers
c) Plate and frame heat exchangers
d-Cooling Towers
d-Cooling Towers
Overall heat transfer coefficient
1
𝑈𝑜𝐴𝑜 = 1
ℎ𝑖𝜂𝑖𝐴𝑖 + 𝑅𝑓𝑖′′
𝜂𝑖𝐴𝑖 + 𝑅𝑤 + 𝑅𝑓𝑜′′
𝜂𝑜𝐴𝑜 + 1 ℎ𝑜𝜂𝑜𝐴𝑜
2-Logarethmic Mean Temperature Difference
LMTD
method𝑇
ℎ𝑖𝑇
ℎ𝑜𝑇
𝑐𝑜𝑇
𝑐𝑖𝑞 = ሶ𝑚ℎ(ℎℎ𝑖 − ℎℎ𝑜) 𝑞 = ሶ𝑚ℎ𝐶𝑝,ℎ (𝑇ℎ𝑖 − 𝑇ℎ𝑜) 𝑞 = 𝐶ℎ(𝑇ℎ𝑖 − 𝑇ℎ𝑜)
𝑞 = ሶ𝑚𝑐(ℎ𝑐𝑜 − ℎ𝑐𝑖) 𝑞 = ሶ𝑚𝑐𝐶𝑝,𝑐(𝑇𝑐𝑜 − 𝑇𝑐𝑜) 𝑞 = 𝐶𝑐(𝑇𝑐𝑜 − 𝑇𝑐𝑖) Hot fluid
Cold fluid
𝐶ℎ = ሶ𝑚ℎ𝐶𝑝,ℎ heat capacity rate [W/K] of the hot fluid 𝐶𝑐 = ሶ𝑚𝑐𝐶𝑝,𝑐 heat capacity rate [W/K] of the cold fluid
Temperature distribution
2-Logarethmic Mean Temperature Difference
LMTD
methodHeat transfer for a small element of thickness
dx and heat transfer area of dA
Parallel heat exchanger arrangement
Δ𝑇 = 𝑇ℎ − 𝑇𝑐 𝑑𝑞 = − ሶ𝑚ℎ𝐶𝑝,ℎ𝑑𝑇ℎ = −𝐶ℎ𝑑𝑇ℎ 𝑑𝑞 = ሶ𝑚𝑐𝐶𝑝,𝑐𝑑𝑇𝑐 = 𝐶𝑐𝑑𝑇𝑐
𝑑𝑞 = 𝑈𝑑𝐴(𝑇ℎ − 𝑇𝑐) 𝑑 Δ𝑇 = 𝑑𝑇ℎ − 𝑑𝑇𝑐
𝑑 Δ𝑇 = −𝑑𝑞
𝐶ℎ − 𝑑𝑞 𝐶𝑐
2-Logarethmic Mean Temperature Difference
LMTD
method𝑑 Δ𝑇 = −𝑑𝑞
𝐶ℎ − 𝑑𝑞 𝐶𝑐 𝑑 Δ𝑇 = −𝑑𝑞 1
𝐶ℎ + 1 𝐶𝑐 𝑑𝑞 = 𝑈𝑑𝐴Δ𝑇 𝑑 Δ𝑇 = −𝑈𝑑𝐴Δ𝑇 1
𝐶ℎ + 1 𝐶𝑐 𝑑Δ𝑇
Δ𝑇 = −𝑈𝑑𝐴 1
𝐶ℎ + 1 𝐶𝑐
𝑑Δ𝑇
Δ𝑇 = −𝑈𝑑𝐴 𝑇ℎ𝑖 − 𝑇ℎ𝑜
𝑞 + 𝑇𝑐𝑜 − 𝑇𝑐𝑖 𝑞
𝑞 = 𝐶ℎ(𝑇ℎ𝑖 − 𝑇ℎ𝑜)
𝑞 = 𝐶𝑐(𝑇𝑐𝑜 − 𝑇𝑐𝑖) 𝐶ℎ = 𝑞
𝑇ℎ𝑖 − 𝑇ℎ𝑜
𝐶𝑐 = 𝑞 𝑇𝑐𝑜 − 𝑇𝑐𝑖
𝑑Δ𝑇
Δ𝑇 = −𝑈𝑑𝐴
𝑞 𝑇ℎ𝑖 − 𝑇𝑐𝑖 − 𝑇ℎ𝑜 − 𝑇𝑐𝑜
ln Δ𝑇2
Δ𝑇1 = 𝑈𝐴
𝑞 𝑇ℎ𝑜 − 𝑇𝑐𝑜 − 𝑇ℎ𝑖 − 𝑇𝑐𝑖
Δ𝑇2 = 𝑇ℎ𝑜 − 𝑇𝑐𝑜 Δ𝑇1 = (𝑇ℎ𝑖−𝑇𝑐𝑜) 𝑞 = 𝑈𝐴 Δ𝑇2 − Δ𝑇1
ln(Δ𝑇2ΤΔ𝑇1) 𝑞 = 𝑈𝐴Δ𝑇𝑙𝑚
2-Logarethmic Mean Temperature Difference
LMTD
methodΔ𝑇𝑙𝑚 = 𝐿𝑀𝑇𝐷
Logarithmic Mean Temperature Difference LMTD
In general
𝑞 = 𝑈𝐴Δ𝑇
𝑙𝑚F is the correction factor
F=1 for the following cases:
a) Pure counter current flow b) Pure parallel flow
c) Evaporators (phase change) d) Condensers (phase change)
Δ𝑇
𝑙𝑚= Δ𝑇
𝑙𝑚,𝐶𝐹𝐹
Δ𝑇𝑙𝑚 is called Logarithmic Mean Temperature
Difference=LMTD
For other geometries, see the next slides
2-Logarethmic Mean Temperature Difference
LMTD
methodRef.: Cengle heat transfer an engineering approach, 2nd edition
LMTD correction factor
Ref.: Cengle heat transfer an engineering approach, 2nd edition
LMTD correction factor
Ref.: Cengle heat transfer an engineering approach, 2nd edition
LMTD correction factor
Ref.: Cengle heat transfer an engineering approach, 2nd edition
LMTD correction factor
Special Cases
SIZING PROBLEMS :
• Heat rate q required is known. Outlet temperatures can be calculated.
• Calculate DT
lm,CFand obtain the correction factor (F) if necessary
• Calculate the overall heat transfer coefficient, U.
• Determine A using 𝑞 = 𝑈𝐴ΔT
LM,CFF
The LMTD method is not as easy to use for performance analysis….
LMTD Method
Example 11.1
Example 11.1
Example 11.1
Example 11.1
Example 11.1
Heat transfer coefficient Correlations used from Ch.8 a-Turbulent flow inside a pipe
b-Laminar flow inside an annulus
𝜖 = 𝑓(𝐶
𝑟, 𝑁𝑇𝑈) 𝑁𝑇𝑈 = 𝑓(𝐶
𝑟, 𝜖)
𝐶𝑟 = 𝐶𝑚𝑖𝑛 𝐶𝑚𝑎𝑥
NTU =Number of heat transfer units 𝑁𝑇𝑈 = 𝑈𝐴 𝐶𝑚𝑖𝑛 𝑞𝑚𝑎𝑥 = 𝐶𝑚𝑖𝑛Δ𝑇𝑚𝑎𝑥 = 𝐶𝑚𝑖𝑛(𝑇ℎ𝑖 − 𝑇𝑐𝑖)
𝜖 = 𝑞
𝑞𝑚𝑎𝑥
𝑞 = 𝑞
𝑚𝑎𝑥𝜖
Heat Exchanger effectiveness
𝜖 − 𝑁𝑇𝑈 Method
Define the maximum possible heat
Define the maximum and minimum heat capacity rate
𝐶𝑚𝑖𝑛 = 𝑚𝐶ሶ 𝑝 𝑚𝑖𝑛 𝐶𝑚𝑎𝑥 = 𝑚𝐶ሶ 𝑝 𝑚𝑎𝑥
𝜖 − 𝑁𝑇𝑈 Method
Assume Ch=Cmin
𝜖 = 𝑞
𝑞𝑚𝑎𝑥 = 𝐶ℎ(𝑇ℎ𝑖 − 𝑇ℎ𝑜) 𝐶ℎ(𝑇ℎ𝑖 − 𝑇𝑐𝑖)
Consider counter current heat exchanger
From LMTD analysis
Effectiveness as a function of C
rand NTU
NTU relations as a function of and Cr for different heat exchangers
𝜖 − 𝑁𝑇𝑈
𝜖 − 𝑁𝑇𝑈
𝜖 − 𝑁𝑇𝑈
Cross flow heat exchanger Both fluid un-mixed
Cross flow heat exchanger One fluid mixed and the other un-mixed
PERFORMANCE ANALYSIS
• Usually inlet temperatures, mass flow rates and heat
exchanger area A, are known. Calculate the capacity ratio C
r= C
min/C
maxand NTU = UA/C
minfrom input data
• Determine the effectiveness from the appropriate charts or
-NTU equations for the given heat exchanger and specified flow arrangement.
• When is known, calculate the total heat transfer rate using 𝜀 =
𝑞𝑞𝑚𝑎𝑥
, where 𝑞
𝑚𝑎𝑥= 𝐶
𝑚𝑖𝑛Δ𝑇
𝑚𝑎𝑥• Calculate the outlet temperature.
𝜖 − 𝑁𝑇𝑈
Example 11.3
Example 11.3
Example 11.3
Example 11.3
Example 11.3
Compact heat exchangers
MEP460
Heat Exchanger Design
Ch. 11 Incropera, 6
thEdition
Feb. 2018
Compact heat exchangers
Surface heat transfer area over volume 𝛼
Tube fin compact heat exchangers
Tube fin compact heat exchangers
Plat fin compact heat exchangers
Heat transfer and pressure drop for tube fin heat exchangers
1
𝑈𝑜𝐴𝑜 = 1
ℎ𝑖𝜂𝑖𝐴𝑖 + 𝑅𝑓𝑖′′
𝜂𝑖𝐴𝑖 + 𝑅𝑤 + 𝑅𝑓𝑜′′
𝜂𝑜𝐴𝑜 + 1 ℎ𝑜𝜂𝑜𝐴𝑜
Chapter 8 can be used to find the heat transfer coefficient inside pipes or ducts
For ho outside (gas) heat transfer coefficient use Kays & London book in compact heat exchangers
𝜂𝑜 = 1 − 𝐴𝑓
𝐴 (1 − 𝜂𝑓)
Overall surface efficiency 𝜂𝑜
𝜂𝑓 is the fin efficiency
Definitions
Frontal area A
frFree Flow area A
ffFin area/total area=A
f/A
o𝜎 = 𝐹𝑟𝑒𝑒 𝑓𝑙𝑜𝑤 𝑎𝑟𝑒𝑎
𝐹𝑟𝑜𝑛𝑡𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝐴𝑓𝑓 𝐴𝑓𝑟
𝛼 = Surface area/Volume
Definitions
Colburn j
Hfactor 𝑗
𝐻= 𝑆𝑡𝑃𝑟
2 3Τ𝑆𝑡 = 𝑁𝑢
𝑅𝑒 𝑃𝑟 = ℎ
𝜌𝐶𝑝𝑉𝑚𝑎𝑥 = ℎ 𝐶𝑝𝐺
Mass velocity [kg/(m
2.s)
𝐺 = 𝜌𝑉𝑚𝑎𝑥 = 𝜌𝑉𝐴𝑓𝑟𝐴𝑓𝑓 = 𝑚ሶ
𝐴𝑓𝑓 = 𝑚ሶ 𝜎𝐴𝑓𝑟
Stanton Number
Friction factor f
Δ𝑃 = 𝑓 𝐿𝐷 𝜌 𝑉2 2
𝑅𝑒 = 𝐺𝐷
ℎ/𝜇
𝑣𝑚 = 𝑣𝑖 + 𝑣𝑜 2 𝐴
𝐴𝑓𝑓 = 𝛼𝑉 𝜎𝐴𝑓𝑟 A: heat transfer area
Afr Frontal area Aff Free flow area
𝜎 = 𝐹𝑖𝑛 𝑎𝑟𝑒𝑎
𝑇𝑜𝑡𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝐴𝑓 𝐴
𝛼 = 𝐴 𝑉
Pressure drop gas side
𝑣
𝑖specifc volume at inlet 𝑣
𝑜specific volume at outlet
𝑣
𝑚mean specific volume =
𝑣𝑖+𝑣𝑜2
Surface information (CF-7.0-5/8J)
Circular fin on circular tubes
Typical data for tube fin heat exchangers (8.0-3/8T)
Continuous fin on circular tubes
𝐹𝑖𝑛 𝑎𝑟𝑒𝑎
𝑇𝑜𝑡𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝐴
𝑓𝐴
𝛼 = 𝐴 Surface density 𝑉
Surface information
Hydraulic diameter Dh
𝜎 = 𝐹𝑟𝑒𝑒 𝑓𝑙𝑜𝑤 𝑎𝑟𝑒𝑎
𝐹𝑟𝑜𝑛𝑡𝑎𝑙 𝑎𝑟𝑒𝑎 = 𝐴𝑓𝑓 𝐴𝑓𝑟
Surface information
1
𝑈𝑜𝐴𝑜 = 1
ℎ𝑖𝜂𝑖𝐴𝑖 + 𝑅𝑓𝑖′′
𝜂𝑖𝐴𝑖 + 𝑅𝑤 + 𝑅𝑓𝑜′′
𝜂𝑜𝐴𝑜 + 1 ℎ𝑜𝜂𝑜𝐴𝑜
1
𝑈𝑜 = 1
ℎ𝑖( Τ𝐴𝑖 𝐴𝑜) + 𝐴𝑜𝑙𝑛( Τ𝑟𝑜 𝑟𝑖)
2𝜋𝑘𝐿 + 1 ℎ𝑜𝜂𝑜
Need to know the heat transfer area ratio
Evaluating overall heat transfer coefficient
Neglecting fouling resistances
𝑅𝑤 = ln( Τ𝑟𝑜 𝑟𝑖) 2𝜋𝑘𝐿
1
𝑈𝑜 = 1
ℎ𝑖( Τ𝐴𝑖 𝐴𝑜) + 𝐷𝑖𝑙𝑛( Τ𝑟𝑜 𝑟𝑖)
2𝑘 ( Τ𝐴𝑖 𝐴𝑜) + 1 ℎ𝑜𝜂𝑜
Ratio of inside to outside heat transfer area
𝐴𝑖 = 𝜋𝐷𝑖𝐿 𝐴𝑜,𝑝 = 𝜋𝐷𝑜𝐿
𝐴𝑜 = 𝐴𝑢𝑓 + 𝐴𝑓 = 𝐴𝑜,𝑝 + 𝐴𝑓 𝐴𝑖
𝐴𝑜,𝑝 = 𝐷𝑖 𝐷𝑜
𝐴𝑜,𝑝 = 𝐴𝑜 − 𝐴𝑓 𝐴𝑖
𝐴𝑜 = 𝐷𝑖
𝐷𝑜 ∗ 1 − 𝐴𝑓 𝐴𝑜 𝐴𝑖 = 𝐷𝑖
𝐷𝑜 𝐴𝑜,𝑝
D
oD
iFins
Inside heat transfer area Outside heat transfer area without fins
Neglecting the area occupied by fins. i.e. Auf=Aop
Example 11.6 Continue
Example 11.6 Continue
Example 11.6 Continue
𝑅𝑒 = 𝐺𝐷ℎ 𝜇