化工原理英文教材 传热 无相变传热Heat transfer to fluids without phase change课件.ppt
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1、化工原理化工原理PrinciplesofChemicalIndustryHeat transfer to fluids without phase changeRegimes of heat transfer in fluidsA fluid being heated or cooled may be flowing in different flow patterns.Also,the fluid may be flowing in forced or natural convection.At ordinary velocities the heat generated from flui
2、d friction is negligible in comparison with the heat transferred between the fluids.Because the situations of flow at the entrance to a tube differs from those well downstream from the entrance,the velocity field and associated temperature field may depend on the distance from the tube entranceThe p
3、roperties of the fluid-viscosity,thermal conductivity,specific heat,and density are important parameters in heat transfer.Each of these,especially viscosity,is temperature-dependent.Heat transfer by forced convection in turbulent flowPerhaps the most important situation in heat transfer is the heat
4、flow in a stream of fluid in turbulent flow.Since the rate of heat transfer is greater in turbulent flow than in laminar flow,most equipment is operated in the turbulent range.A dimensional analysis of the heat flow to a fluid in turbulent flow through a straight pipe yields dimensionless relations.
5、(12-27),pchddufk The three groups in Eq(12-27)are recognized as the Nusselt(Nu),Reynolds(Re),and Prandtl(Pr)numbers respectively.The Nusselt number for heat transfer from a fluid to a pipe or from a pipe to a fluid equals the film coefficient multiplied by d/kThe film coefficient h is the average va
6、lue over the length of the pipehdNuk Prandtl number Pr is the ratio of the diffusivity of momentum/to the thermal diffusivity k/cpPrpck The Prandtl number of a gas is usually close to 1(0.69 for air,1.06 for steam).The Prandtl number of gases is almost independent of temperature because the viscosit
7、y and thermal conductivity both increase with temperature at about the same rate.Empirical equationFor heat transfer to and from fluids that follow the power-law relation,the dimensionless relation becomesTo use the dimensionless relation,the constant c and index m,n must be known.()()pmnchdduckk A
8、recognized empirical correlation,for long tubes with sharp-edged entrances,is the Dittus-Boelter equation Where n is 0.4 when the fluid is being heated and 0.3 when it is being cooled.0.80.023RePrnihdNuk A better relationship for turbulent flow is known as the Sieder-Tate equation (12-32)0.81/30.140
9、.023RePr()wNu Equation(12-32)should not be used for Reynolds numbers below 6000 or for molten metals,which have abnormally low Prandtl number.Effect of tube lengthNear the tube entrance,where the temperature gradients are still forming,the local coefficient hx is greater than h for fully developed f
10、low.In entrance,hx is quite large,but hx value drops rapidly toward h in a comparatively short length of tube.Average value of hi in turbulent flow.Since the temperature of the fluid changes from one end of the tube to the other and fluid properties ,cp and k are all function of temperature,the loca
11、l value of hi also varies from point to point along the tube.The relation of local heat transfer coefficient hi and long tube h is as followsWhen L approaches infinite,hi is close to the h of long tube.7.0)(1/LDhhiFor laminar flow,the relation of Nu and Pr and Re is (12.25)3/1Pr)(ReANu For gases the
12、 effect of temperature on hi is small.The increase in conductivity and heat capacity with temperature offset the rise in viscosity,giving a slight increase in hi.For liquids the effect of temperature is much greater than for gases because of the rapid decrease in viscosity with rising temperature.Th
13、e effects of k,cp,and in Eq(12-36)all act in the same direction,but the increase in hi with temperature is due mainly to the effect of temperature on viscosity.In practice,an average value of hi is calculated and used as a constant in calculating the overall coefficient U.the average value of hi is
14、computed by evaluating the fluid properties k,cp,and at average fluid temperature,defined as the arithmetic mean between the inlet and outlet temperatures.Estimation of wall temperature tw The estimation of tw requires an iterative calculation based on the resistance equation111mowiooooimitTttddbUhk
15、 dh d To determine tw the wall resistance can usually be neglected11miooiittdUh dSubstituting Uo,gives (12-38)111iimiioohttdhh d Cross sections other than circular To use Eq(12-30)for cross section other than circular it is only necessary to replace the diameter in both Reynolds and Nusselt number b
16、y the equivalent diameter de.de is defined as 4 times the hydraulic radius rH.The method is the same as that used in calculating friction loss.Heat transfer in transition region between laminar and turbulent flow Equation(12-32)applies only for Reynolds numbers greater than 6000.The range of Reynold
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