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Diffstat (limited to '2510/CH10/EX10.6')
-rwxr-xr-x | 2510/CH10/EX10.6/Ex10_6.sce | 29 |
1 files changed, 29 insertions, 0 deletions
diff --git a/2510/CH10/EX10.6/Ex10_6.sce b/2510/CH10/EX10.6/Ex10_6.sce new file mode 100755 index 000000000..85a5e7a26 --- /dev/null +++ b/2510/CH10/EX10.6/Ex10_6.sce @@ -0,0 +1,29 @@ +//Variable declaration: +Ts = 200.0+460.0 //Surface temperature of pipe (°R) +Too = 70.0+460.0 //Air temperature (°R) +D = 0.5 //Diameter of pipe (ft) +R = 0.73 //Universal gas constant (ft^3.atm.R^−1.lb.mol^−1) +P = 1.0 //Atmospheric pressure (Pa) +MW = 29.0 //Molecular weight of fluid (mol) +//From Appendix: +mu = 1.28*10**-5 //Absolute viscosity (lb/ft.s) +k = 0.016/3600.0 //Thermal conductivity (Btu/s.ft.°F) +g = 32.174 //Gravitational acceleration (ft/s^2) + +//Calculation: +Tav = (Ts+Too)/2 //Average temperature (°R) +v = R*Tav/P //kinematic viscosity (ft^3/lbmol) +p = MW/v //Air density (lb/ft^3) +B = 1.0/Tav //Coefficient of expansion (°R^-1) +DT = Ts-Too //Temperature difference (°R) +Gr = D**3*p**2*g*B*DT/mu**2 //Grashof number +//From equation 10.5: +Cp = 0.25 //Air heat capacity (Btu/lb.°F) +Pr = Cp*mu/k //Prandtl number +GrPr = 10**8.24 //Rayleigh number +//From Holman^(3): +Nu = 10**(1.5) //Nusselt number +h = Nu*(k/D)*3600.0 //Air heat transfer film coefficient (Btu/h.ft.°F) + +//Result: +printf("The required air heat transfer film coefficient is : %.2f Btu/h.ft.°F .",h) |