Lecture 17-Hex.pptx: heat excanger: theories and practice

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About This Presentation

Descript heat exchager theories and use. Calculation means log temperature . Coefficient of excanger. power of heat excanger . Type of heat exger. balance. Renolds . NUT,


Slide Content

Heat Exchangers Chapter 11 Section 11.5 Lecture 17

4. Effectiveness – NTU Method New Definitions Fluid Heat Capacity Rates

Effectiveness – NTU Method New Definitions Effectiveness: N umber of T ransfer U nits:

Effectiveness – NTU Method For Parallel Flow with C min = C h

Effectiveness – NTU Method For Parallel Flow with C min = C h

Effectiveness – NTU Method For Counterflow with C r = C min /C max

Effectiveness – NTU Method For Counterflow with C r = C min /C max

tbl_11_03

tbl_11_04

Effectiveness – NTU Method Graphical Representations of Equations in Tables 11.3 & 11.4

Effectiveness – NTU Method

Effectiveness – NTU Method

5. Methodology for Heat Exchanger Calculation Heat Exchanger Design -- LOG-Mean Known: Fluid flow rates and Ts Find: Heat exchanger size (Area) Heat Exchanger Performance Calculation Known: Heat Exchanger Size Find: Heat transfer rate and fluid outlet Ts ε -NTU method is useful for performance calculation

LOG-Mean Method Calculate unknown fluid T from energy balance ; Calculate  T lm or  T lm,CF ; Calculate P and R, find F value; Calculate q from energy balance equation; Determine A from q/(UF  T lm,CF )

Counterflow Heat Exchanger

Multipass and Cross-flow Heat Exchanger F for different flow arrangements can be found in figures 11S.1-11S.4

Effectiveness – NTU Method Calculate C h and C c , determine C min /C max ; Calculate NTU from UA/C min , find ε ; Calculate q max = C min * (T h,i -T c,i ); Calculate q = ε * q max ; Determine unknown fluid outlet Ts.

Effectiveness – NTU Method Calculate C h and C c , determine C min /C max ; Calculate q max ; Calculate q and ε ; Get NTU from the chart or equation; Determine A from NTU.

Effectiveness – NTU Method For Counterflow with C r = C min /C max

Effectiveness – NTU Method For Counterflow with C r = C min /C max

Example 11.3 Hot exhaust gases, which enter a finned-tube, cross-flow heat exchanger at 300 C and leave at 100 C, are used to heat pressurized water at a flow rate of 1 kg/s from 35 to 125 C. The exhaust gas specific heat is approximately 1000 J/kgK, and the overall transfer coefficient based on the gas-side surface area is U h = 100 W/m 2 K. Determine the required gas-side surface area A h using both NTU and log-mean methods.

Example 11.3 Known: Hot and cold fluid inlet and outlet Ts, cold fluid flow rates, and hot fluid side overall heat transfer coefficient for a cross-flow heat exchanger Find: Required hot fluid surface area Schematic:

Example 11.3 Assumptions: Negligible heat loss to environment Negligible kinetic and potential energy changes Constant properties Properties: For water, find c p value from Table A.6 For exhaust gases, c p =1000 J/kgK is given

Example 11.3 Analysis: NTU Method 1. Calculate C min and C max , but is unknown

Example 11.3 C h was obtained from energy balance equations 2. Calculate q max 3. Calculate q and ε

Example 11.3 4. Find NTU from the chart ( ε =0.75, C r =0.45) Figure 11.18, NTU=2.1 5. Find A h from NTU

Example 11.3 Log-Mean Method 1. Calculate  T lm,CF = 111 C 2. Calculate P and R, find F from Fig. 11S.2 P=(t o -t i )/(T i -t i )=0.34, R =(T i -T o )/(t o -t i )=2.22 F ≈ 0.87

Example 11.3 3. Calculate A h

Example 11.4 Consider Example 11.3, the overall transfer coefficient is U h = 100 W/m 2 K and area of 40 m 2 . The water flow rate and inlet temperature remain at 1 kg/s and 35 C. However, a change in operating conditions for hot gas generator causes the gases to now enter the heat exchanger with a flow rate of 1.5 kg/s and a temperature of 250C. What is the rate of heat transfer by the exchanger, and what are the gas and water outlet temperatures?

Example 11.4 Known: Hot and cold fluid inlet conditions for a finned-tube cross-flow heat exchanger of known surface area and overall heat transfer coefficient. Find: Heat transfer rate and fluid outlet Ts. Schematic:

Example 11.4 Assumptions: Negligible heat loss to environment Negligible kinetic and potential energy changes Constant properties Properties: For water, find c p value from Table A.6 For exhaust gases, c p =1000 J/kgK is given

Example 11.4 Analysis: NTU Method 1. Calculate C min and C max ,

Example 11.4 2. Calculate NTU and find ε Find ε to be 0.82 from Figure 11.14 3. Calculate q max

Example 11.4 4. Calculate q q = q max * ε =2.65x10 5 W 5. Calculate T h,o and T c,o

Example 11.5 The condenser of a large steam power plant is a heat exchanger in which steam is condensed to liquid water. Assume the condenser to be a shell-tube heat exchanger consisting of a single shell an 30,000 tubes, each executing two passes. The tubes are of thin wall construction with D=25 mm, and steam condenses on their outer surface with an associated convection coefficient of h o =11,000 W/m 2 K.

Example 11.5 The heat transfer rate that must be effected by the exchanger is q=2x10 9 W, and this is accomplished by passing cooling water through the tubes at a rate of 3x10 4 kg/s (the flow rate per tube is therefore 1 kg/s). The water enters at 20 C, while the steam condenses at 50 C. What is the temperature of the cooling water emerging from the condenser? What is the required tube length L per pass?

Example 11.5 Known: Heat exchanger of a single shell and double tube passes with 30,000 tubes Find: Outlet T of cooling water, Tube length per pass to achieve the required heat transfer. Schematic:

Example 11.5 Assumptions: Negligible heat loss to environment Negligible kinetic and potential energy changes Constant properties Fully developed conditions for internal flow Negligible thermal resistance through the tube wall and fouling Properties: For water, find c p , μ and k, Pr values from Table A.6 Assume the average cooling water temperature at 300K

Example 11.5 Analysis: Calculate T c,o from energy balance 2. Heat exchanger design calculation using LMTD or NTU method where A = N*2L*  D, U=(1/h i +1/h o ) -1

Example 11.5 3. Estimate h i from internal flow correlations Calculate U = (1/h i +1/h o ) -1 = 4478 W/m 2 K Calculate  T lm,CF h i = 7552 W/m 2 K

Example 11.5 6. Calculate L F was determined from Fig. 11S.1, P=0.53, R=0, F=1

Example 11.5 7. NTU method C h =C max = ,

Example 11.5 7. From Figure 11.12, we get NTU =0.75 (C r =0, and  =0.53) NTU = UA/C min A=N2  DL, U=4478 W/m 2 K L = NTU * C min /(2*U*N* * D) = 4.66 m