printf("\t example 15.5\n"); printf("\t approximate values are mentioned in the book \n"); W=40800; // lb/hr w=4570; // lb/hr printf("\t 1.for heat balance \n"); Ht1=241; // enthalpy of liquid at 228F, Btu/lb, fig 9 Ht2=338; // enthalpy of vapourat 228F, Btu/lb, fig 9 Q=(W*(Ht2-Ht1)); printf("\t total heat required for butane is : %.2e Btu/hr \n",Q); l=868; // Btu/(lb), table 7 Q=((w)*(l)); // Btu/hr printf("\t total heat required for steam is : %.2e Btu/hr \n",Q); delt=125; // delt=LMTD, isothermal boiling, eq 5.14 // Tc and tc: Both streams are isuthermal printf("\t trail 1 \n"); A1=((Q)/((12000))); // Q/A1 =12000, first trial should always be taken for the maximum allowable flux printf("\t A1 is : %.1e ft^2 \n",A1); a1=0.1963; // ft^2/lin ft L=16; N1=(A1/(L*a1)); // table 10 printf("\t number of tubes are : %.0f \n",N1); N2=109; // assuming one tube passes, 13.25-in ID, from table 9 A2=(N2*L*a1); // ft^2 printf("\t total surface area is : %.0f ft^2 \n",A2); UD=((Q)/((A2)*(delt))); printf("\t correct design overall coefficient is : %.1f Btu/(hr)*(ft^2)*(F) \n",UD); // Assume 4: 1 recirculation ratio rowv=(58/(359*(688/492)*(14.7/290))); // eq 15.18 printf("\t vapour density : %.2f lb/ft^3 \n",rowv); Vv=0.44; Vl=0.0372; // fig 6 W1=4*W; printf("\t weight flow of recirculated liquid : %.3e lb/hr \n",W1); VL=W1*Vl; VV=W*Vv; printf("\t volume of liquid : %.2e ft^3 \n",VL); printf("\t volume of vapour : %.3e ft^3 \n",VV); V=VL+VV; printf("\t total volume out of reboiler : %.3e ft^3 \n",V); vo=(V/(W1+W)); printf("\t vo is : %.4f ft^3/lb \n",vo); Pl=((2.3*16)/(144*(vo-Vl)))*(log10(vo/Vl)); printf("\t pressure leg : %.1f psi \n",Pl); printf("\t frictional resistance \n"); Nt=109; n=1; // number of passes at1=0.302; // flow area,table 10, in^2 at=((Nt*at1)/(144*n)); // total area,ft^2,from eq.7.48 printf("\t flow area is : %.3f ft^2 \n",at); Gt=((W1+W)/(at)); // mass velocity,lb/(hr)*(ft^2) printf("\t mass velocity is : %.2e lb/(hr)*(ft^2) \n",Gt); mu1=0.242; // at 228F, fig 14,lb/(ft)*(hr) D=0.0517; // ft Ret=((D)*(Gt)/mu1); // reynolds number printf("\t reynolds number is : %.1e \n",Ret); f=0.000127; // using fig.26 s=0.285; phyt=1; delPt=((f*(Gt^2)*(L)*(n))/(5.22*(10^10)*(D)*(s)*(phyt))); // using eq.7.45,psi printf("\t delPt is : %.2f psi \n",delPt); P=Pl+delPt; printf("\t total resisitance : %.2f psi \n",P); F=(16*0.43*62.5/144); printf("\t driving force : %.2f psi \n",F); // The resistances are greater than the hydrostatic head can provide; hence the recirculation ratio will be less than 4: 1 printf("\t trial 2 \n"); // Assume 12'0" tubes and 4:1 recirculation ratio A1=((Q)/((12000))); // Q/A1 =12000, first trial should always be taken for the maximum allowable flux printf("\t A1 is : %.1e ft^2 \n",A1); a1=0.1963; // ft^2/lin ft L=12; N1=(A1/(L*a1)); // table 10 printf("\t number of tubes are : %.0f \n",N1); N2=151; // assuming one tube passes, 15.25-in ID, from table 9 A2=(N2*L*a1); // ft^2 printf("\t total surface area is : %.0f ft^2 \n",A2); UD=((Q)/((A2)*(delt))); printf("\t correct design overall coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",UD); Pl=((2.3*12)/(144*(vo-Vl)))*(log10(vo/Vl)); printf("\t pressure leg : %.1f psi \n",Pl); printf("\t frictional resistance \n"); Nt=151; n=1; // number of passes at1=0.302; // flow area,table 10, in^2 at=((Nt*at1)/(144*n)); // total area,ft^2,from eq.7.48 printf("\t flow area is : %.3f ft^2 \n",at); Gt=((W1+W)/(at)); // mass velocity,lb/(hr)*(ft^2) printf("\t mass velocity is : %.2e lb/(hr)*(ft^2) \n",Gt); mu1=0.242; // at 228F, fig 14,lb/(ft)*(hr) D=0.0517; // ft Ret=((D)*(Gt)/mu1); // reynolds number printf("\t reynolds number is : %.2e \n",Ret); f=0.000135; // using fig.26 s=0.285; phyt=1; delPt=((f*(Gt^2)*(12)*(n))/(5.22*(10^10)*(D)*(s)*(phyt))); // using eq.7.45,psi printf("\t delPt is : %.2f psi \n",delPt); P=Pl+delPt; printf("\t total resisitance : %.2f psi \n",P); F=(12*0.43*62.5/144); printf("\t driving force : %.2f psi \n",F); // Since the driving force is slightly greater than the resistances, a recirculation ratio better than 4:1 is assured. printf("\t hot fluid : shell side,steam \n"); ho=1500; // condensing steam printf("\t cold fluid:inner tube side, butane \n"); jH=330; // from fig.24 Z=0.115; // Z=k*((c)*(mu1)/k)^(1/3), fig 16 Hi=((jH)*(1/D)*(Z)); //, Hi=(hi/phyt)using eq.6.15d,Btu/(hr)*(ft^2)*(F) printf("\t individual heat transfer coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",Hi); Hio=((300)*(0.62/0.75)); //Hio=(hio/phyp), using eq.6.9 printf("\t Correct Hio to the surface at the OD is : %.0f Btu/(hr)*(ft^2)*(F) \n",Hio); Uc=((Hio)*(ho)/(Hio+ho)); // clean overall coefficient,Btu/(hr)*(ft^2)*(F) printf("\t clean overall coefficient is : %.0f Btu/(hr)*(ft^2)*(F) \n",Uc); UD=89; Rd=((Uc-UD)/((UD)*(Uc))); // (hr)*(ft^2)*(F)/Btu printf("\t actual Rd is : %.4f (hr)*(ft^2)*(F)/Btu \n",Rd); // end