shell and tube heat exchanger1

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Shell and Tube Heat Exchanger Project: Evaporator Item No.: - Service: Cooling of 23% sodium chloride solution Tube Side Shell R-404 Fluid Name odium Chloride 1.132 Flow (M), Kg/s 33.2 -13 -9 -13 -10 Av. Density 903 1050 Av. Viscosity 0.158 2.300 Av. Heat Capacity 1.250 4.36 Heat Exchanged 145 Q, kW 145 hermal Conductivity 0.0376 0.5800 Fouling Resistance 0.0004 0.0004 LMTD 3.5 Corrected LMTD 3.5 Tube OD 0.0125 m length (can be trial and error BWG 16 Tube ID, d = 0.00925 m Tube Length, L = 2 m Area of one tube = 0.079 Cross sectional area of tube = 0.00007 page number 648 Bundle diameter = 0.417758 m Shell diameter = 0.430258 m 7382 Prandtl No. = 5.24 Length / ID = 216 page number 665 0.0032 Nusselt number = 40.80 165.86 The values in this block will keep on changing Step 1. Input flows, conditions and properties data for shellside and tubeside Temp. in, °C Temp. out, °C r, Kg/m 3 m, mNs/m 2 cp, kJ/kg°C k, W/m°C R,m² °C/W °C °C Step 2. Input tubing OD, BWG and Step. 4 Bundle and Shell diameter Step. 5 Tube side heat transfer coefficient Tubeside Reynolds No., NRe = j h h i = W/m² °C

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Shell and Tube HX for 4 TRShell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Cooling of 23% sodium chloride solutionBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 3. Start configuring the exchanger. Begin with the assumed overall heat transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =1000.00W/m C110.1200.014R-404Fluid NameSodium ChlorideThen the required transfer A =41.714m2120.1090.0111.132Flow (M), Kg/s33.2Number of tubes required =531130.0950.014-13Temp. in, C-9No. of passes =4140.0830.012-13Temp. out, C-10Tubes per pass =134132.85150.0720.011Av. Density903r, Kg/m31050Area of tubes per pass =0.00900m160.0650.007Av. Viscosity0.158m, mNs/m22.300Volumetric flow =0.001254m/sAv. Heat Capacity1.250cp, kJ/kgC4.36Av. Velocity =0.139284m/sHeat Exchanged145Q, kW145Av. Thermal Conductivity0.0376k, W/mC0.5800Fouling Resistance0.0004R,m C/W0.0004Step 6. Shell side heat transfer coefficientTube Pitch =0.015625mPattern =Tri.LMTD3.5CBaffle Spacing =0.237mCorrected LMTD3.5CArea of Shell =0.020363mEquivalent Diameter, de =0.008876mVolumetric flowrate =0.031660m/sStep 2. Input tubing OD, BWG andTube OD0.0125mShellside velocity =1.55m/slength (can be trial and error).BWG16Shellside Reynolds No., NRe =6,300Tube ID, d =0.00925mPrandtl No. =17Tube Length, L =2mSegmental baffle cut 25% page number 673 jh =0.0070Area of one tube =0.079mNusselt number =114Cross sectional area of tube =0.00007mho =7,444W/m CR1 =0.00013For 2 t.pFor 4 t.pFor 6 t.pR2 =0.00040For 2 tube passesk10.2490.1750.0743page number 649Step. 4 Bundle and Shell diameterpage number 648Bundle diameter =0.417758mR3 =0.000042n12.2072.2852.499page number 649Shell diameter =0.430258mR4 =0.0087Clearance0.0125page number 646Step. 5 Tube side heat transfer coefficientTubeside Reynolds No., NRe =7382Overall heat transfer coefficient =107.9W/m CPrandtl No. =5.24Length / ID =216page number 665j h0.0032Nusselt number =40.80hi =165.86W/m CThe values in this block will keep on changing

Sheet3Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet4Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet5Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet6Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet7Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet8Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet9Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.

Sheet10Shell and Tube Heat Exchanger Design SpreadsheetProject:EvaporatorProject No.:-Item No.:-Service:Water coolerBy:MASDate/Time:19-Sep-119:40BWG/Tube Wall Thicknesses80.165Step 1. Input flows, conditions and properties data for shellside and tubesideStep 5. Start configuring the exchanger. Begin with the total calculated transfer coefficient to this point:90.1480.017100.1340.014TubeSideShellUstart =10Btu/hft2oF110.1200.014R-22Fluid NameWaterOver all heat transfer Coefficient, Uo =9.7Btu/hft2oF120.1090.011168.5Flow (M), lb/h11,014.1Then the required transfer A =63ft2130.0950.0145Temp. in, oF86Number of tubes required =239140.0830.0125Temp. out, oF82Reset tubes/pass (Step 3), then no. of passes =2150.0720.011Av. Density0.8053r, lb/ft362.42Total tube count =132160.0650.007Av. Viscosity0.011m, cP1.903Tubeside DP (incl. returns) =5.802psiAv. Heat Capacity0.163cp, Btu/lboF1.003Actual effective transfer area, A =35ft2MTD Correction FactorsHeat Exchanged48,000Q, Btu/h44,188Av. Thermal Conductivity0.0049k, Btu/hftoF0.3351R = ( T1 - T2 ) / ( t2 - t1 ) =0.000Fouling Resistance0.0040R, ft2hoF/Btu0.004Step 4. Select tube arrangementTube Pitch0.65in.Prandtl No.0.87cpm/k13.78and estimate shell diameterPatternTri.S = ( t2 - t1 ) / ( T1 - t1 ) =0.000Corrected MTD79.0oFShell ID from Tube Count Tables8in.Corrected MTD79.0oFSelect Baffle Spacing5in.( R2 + 1 ) =0.000Number of Baffles =43.80Flow Area across Bundle, as =0.064ft2( 1 - S ) / ( 1 - RS ) =0.000Step 2. Input tubing OD, BWG andTube OD0.5000in.Equivalent Diameter, de (see table) =7.5in.length (can be trial and error).BWG16Mass Velocity, Gs =171,820lb/hft22 - S ( R + 1 - ( R2 + 1 ) ) =0.000Tube ID, d =0.370in.Shellside Reynolds No., NRe =56,431Tube Length, L =2ft.Shellside Friction Factor =0.001532 - S ( R + 1 + ( R2 + 1 ) ) =0.000Flow area per tube, at =0.108in.2Shellside DP =0.357psiEffective transfer area per tube =0.262ft2Outside Transfer Factor, jh =139.7FT =0.000Outside Film Coefficient, ho =179Calculated Uo =9.7Step 3. Estimate the number ofTubes/pass =66Check: % difference, Ucalc. vs Uassum. =0.0%tubes per tube pass.lb/h per tube =3Uclean =10.5lb/h per tube per pass =1.3Av. velocity, fps =1.18Tubeside Reynolds No., NRe =4,025Tubeside Friction Factor, f =0.027Step 6. Check tubeside velocity and DP, shellside DP. If too high or too low,DP per pass, psi =0.00021adjust tube length, number of tubes per pass, number of passes, and/or shellNusselt number, Nr =7.04baffle spacing. Remember to reset shell diameter from tube count tables, asInside Film Coefficient, hi =11required.