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ERT 209 HEAT & MASS TRANSFER Sem 2/ 2010-2011

ERT 209 HEAT & MASS TRANSFER Sem 2/ 2010-2011. Prepared by; Miss Mismisuraya Meor Ahmad School of Bioprocess Engineering University Malaysia Perlis 17 February 2011. Forced Convection. Outlines.

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ERT 209 HEAT & MASS TRANSFER Sem 2/ 2010-2011

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  1. ERT 209HEAT & MASS TRANSFERSem 2/ 2010-2011 Prepared by; Miss Mismisuraya Meor Ahmad School of Bioprocess Engineering University Malaysia Perlis 17 February 2011

  2. Forced Convection

  3. Outlines To examine the methods of calculating convection heat transfer (particularly, the ways of predicting the value of convection heat transfer coefficient, h) • Convection heat transfer requires an energy balance along with an analysis of the fluid dynamics of the problem concern. So that. The discussion will consider; • simple relations of fluid dynamics • Boundary layer analysis Important for basic understanding of convection heat transfer

  4. The region of flow that develops from the leading edge of the plate in which the effects of viscosity  boundary layer (The y position where the boundary layer ends and the velocity become 0.99 of the free-stream value) Initially  the boundary layer development is laminar but at some critical distance from the leading edge (depending on the flow field & fluid properties), small disturbance in the flow begin to become amplified, and a transition process takes place until the flow become turbulent. occurs when  where 

  5. Flat plate For transition between laminar & turbulence Tube Laminar flow Turbulence flow For transition between laminar & turbulence d = Tube diameter

  6. Re. no. (Tube) Other Form: Define the mass velocity as  So that, mass flow rate  The Reynolds no. may also written 

  7. Classification of Fluid Flows Inviscid Flow Although no real fluid is inviscid, in some instance the fluid may be treated as such, and useful to present some of the equation that apply in these circumstances (the flow at a sufficiently large distance from the plate will behave as a nonviscous flow system). or Fundamentally a Dynamic Equation (The Bernoulli equation) Where,

  8. To solve convection heat transfer coefficient, h we have to: • Identify the type of fluid involve to get the fluid properties • State the process

  9. 1) Type of Fluid # Specify the equation of state of fluid  to calculate pressure drop in compressible flow. An ideal gas Where: e = Internal Energy i = Entalpy Gas Where: Air

  10. 2) State the Process Example: Reversible Adiabatic Flow through a nozzle The relation involved which is relating the properties at some points in the flow to the Mach no. & stagnation properties Where: a: Local velocity of sound For an ideal gas: For air behaving as an ideal gas:

  11. Example 5.1: Water flow in a diffuser Water at 20 °C flows at 8 kg/s through the diffuser arrangement shown in Figure, the diameter at section 1 is 3.0 cm and the diameter at section 2 is 7.0 cm. Determine the increase in static pressure between sections 1 and 2. Assume frictionless flow.

  12. Example 5.2: Isentropic Expansion of Air Air at 300 °C and 0.7 Mpa pressure is expanded isentropically from a tank until the velocity is 300 m/s. Determine the static temp., pressure and Mach number of the air at the high-velocity condition. ϒ= 1.4 for air.

  13. Laminar Boundary Layer on Flat Plate From the analytical analysis by making a force and momentum balance on the element yield the momentum equationfor the laminar boundary layer with constant properties. Can be solved for many boundary conditions. For development in this chapter, we shall satisfied with an approximate analysis that furnishes an easier solution without a loss in physical understanding of process involved.

  14. Laminar Boundary Layer on Flat Plate Consider the boundary layer flow system as shown: The free-stream velocity outside the boundary layer is u∞ and the boundary layer thickness is . We wish to make a momentum-and-force balance on the control volume bounded by the plane 1, 2, A-A and the solid wall. The boundary layer thickness, Mass flow rate  Where: So that 

  15. Example 5.3: Mass Flow & Boundary-Layer Thickness Air at 27 °C and 1 atm flows over a flat plate at a speed of 2 m/s. Calculate the boundary-layer thickness at distances of 20 cm and 40 cm from the leading edge of the plate. Calculate the mass flow that enters the boundary layer between x=20 cm and x= 40 cm. The viscosity of air at 27 ° C is 1.85 x 10-5 kg/ m . s. Assume unit depth in the z direction.

  16. The Thermal Boundary layer Exist when temperature gradient are present in the flow. If the fluid properties were constant throughout the flow, an appreciable variation between the wall and free stream condition which is film temp. Tfdefine as: Used Tf to get the fluid properties from properties fluids table

  17. The Thermal Boundary layer The Thermal Boundary layer Consider the system shown  Tw: The temp. of the wall T∞ : The temp. of the fluid outside the thermal boundary layer : Thickness of the thermal boundary layer Basic: convection/conduction hx: Heat transfer coefficient in term of the distance from the leading edge of the plate Case 1 0.6 < Pr < 50 For the plate heated over its entire length Rex Pr > 100 Used the average heat transfer coefficient 

  18. The Thermal Boundary layer Case 2 For the plate heated starts at or Where:

  19. The Thermal Boundary layer Constant Heat Flux  To find the distribution of the plate surface temp. and So that  From these equation, can be produce equation

  20. The energy Equation of the boundary layer (heat flow, q) & the thermal boundary layer (heat flux, qw) To determine heat flow, q and heat flux, q w From energy equation of the boundary layer From energy equation of the thermal boundary layer Heat flow, q Determine: There is an appreciable variation between wall & free stream condition, so that, it is recommended that the properties be evaluated at film temp. 1) Film temp. 2) The properties of fluid at Tf such as kinematic viscosity, thermal conduction coefficient, heat capacity, Prandtle no. 3) Rex at x=xL 0.6 < Pr < 50 4) Nusselt No. Then  Rex Pr > 100

  21. Heat flow, q 5) Heat transfer coefficient, h 6) The average heat transfer coefficient, 7) Heat Flow, Heat flux, qw

  22. Example 5.4: Isothermal Flat Plate Heated Over Entire Length Air at 27 °C and 1 atm flows over a flat plate at a speed of 2 m/s. Calculate the boundary-layer thickness at distances of 20 cm and 40 cm from the leading edge of the plate. Calculate the mass flow that enters the boundary layer between x=20 cm and x= 40 cm. The viscosity of air at 27 ° C is 1.85 x 10-5 kg/ m . s. Assume unit depth in the z direction and the plate is heated over its entire length to a temp. of 60 ° C. Calculate the heat transferred in • The first 20 cm of the plate and • The first 40 cm of the plate.

  23. Example 5.5: Flat Plate with Constant Heat Flux A 1.0 KW heater is constructed of a glass plate with an electrically conducting film that produces a constant heat flux. The plate is 60 cm by 60 cm and placed in an airstream at 27 °C, 1 atm with u∞ = 5 m/s. Calculate • The average temp. different along the plate and • The temperature difference at the trailing edge.

  24. Example 5.6: Plate with Unheated Starting Length A 1.0 KW heater is constructed of a glass plate with an electrically conducting film that produces a constant heat flux. The plate is 60 cm by 60 cm and placed in an airstream at 27 °C, 1 atm with u∞ = 5 m/s. Calculate • The average temp. different along the plate and • The temperature difference at the trailing edge.

  25. Example 5.7: Oil Flow Over Heated Flat Plate Engine oil at 20 °C is forced over a 20-cm-square plate at a velocity of 1.2 m/s. The plate is heated to a uniform temp. of 60 °C. Calculate the heat lost by the plate.

  26. The relation between fluid friction & heat transfer The shear stress at the wall be expressed in term of a friction coefficient, Cf The relation between fluid friction and heat transfer for Laminar flow on a flat plate This is important relation between friction & heat transfer is the drag force (D) which is depends on the average shear stress. The average of shear stress is a friction coeffiecient Cfx Where: Drag Force, D = (shear stress) (Area)

  27. Example 5.8: Drag Force on a Flat Plate Air at 27 °C and 1 atm flows over a flat plate at a speed of 2 m/s. Calculate the boundary-layer thickness at distances of 20 cm and 40 cm from the leading edge of the plate. Calculate the mass flow that enters the boundary layer between x=20 cm and x= 40 cm. The viscosity of air at 27 ° C is 1.85 x 10-5 kg/ m . s. Assume unit depth in the z direction and the plate is heated over its entire length to a temp. of 60 ° C. Compute the drag forced exerted on the first 40 cm of the plate using the analogy between fluid friction and heat transfer

  28. Turbulent-boundary-layer heat transfer (q) 1) Determine either the flow is turbulent region or not. Check based on Re. no. Turbulent Region 2) Heat transfer (q) from the plate is: Where:

  29. Turbulent-boundary-layer thickness ( ) The boundary layer thickness measured when 500000>Re<10000000 The boundary layer is fully turbulent from the ledge of the plate The boundary layer follows a laminar growth pattern up to Rcrit= 5 x 105 and turbulent growth thereafter

  30. Assignment 5 (submit: 22 Feb 2011 before 1400) • Book: J.P. Holman • 5-15 • 5-17 • 5-26 • 5-29 • 5-40

  31. Heat Transfer in Laminar Tube Flow Consider the tube flow system  Aim to calculate the heat transfer under developed flow condition (Laminar Flow) Consider the fluid element derive to get the velocity and temp. distribution

  32. Heat Transfer in Laminar Tube Flow From the analysis, the analytical solution give; The velocity at the center of the tube  The velocity distribution  The temperature distribution 

  33. Total heat transfer in term of bulk- temperature different The total energy added (energy balance)  The heat added, dq can be expressed in term of a bulk temp. different or h; The total heat transfer  Note: When the statement is made that a fluid enters a tube  used the Bulk Temp. to determine fluid properties

  34. The Bulk Temperature In tube flow, convection heat transfer coefficient, h defined by: Where, Tw : The wall temp. Tb : Bulk temp. Why used Tb? • For most tube flow heat transfer problem, the topic is the total energy transferred to the fluid. • At any x position, the temp. that is indicative of the total energy of the flow is an integrated mass energy average temp. over the entire flow area. • The bulk temp. is representative of the total energy of the flow at the particular location

  35. The Bulk Temperature From the analysis, the analytical solution give; The bulk temp  The wall temp  Heat transfer coefficient  Heat transfer coefficient in term of the Nusselt No. 

  36. Heat Transfer in Laminar Tube Flow The relation to used to calculate heat transfer in laminar tube flow (The empirical relation) Fully developed laminar flow in tubes at constant wall temp. # used for long & smooth tube Fully developed laminar flow in tubes at constant wall temp. # used for short & smooth tube # the fluid properties are evaluated at mean bulk temp. of the fluid. Used if  Where: Peclet number (Pe)

  37. Heat Transfer in Laminar Tube Flow For rough tubes (relation fluid friction and heat transfer), expressed in term of the Stanton Number: Where;

  38. Heat Transfer in Laminar Tube Flow To calculated local and average Nusselt No. for laminar entrance regionsfor the case of a fully developed velocity profile used Graph with “inverse Graetz number”

  39. Local & average Nusselt No. for circular tube thermal entrance regions in fully developed laminar flow

  40. Turbulent Flow in a Tube Velocity profile for turbulent flow in a tube  To determine heat transfer analytically  should know the temp. distribution in the flow # to obtain temp. distribution, the analysis must take into consideration the effect of the turbulent eddies in the transfer of heat and momentum)

  41. Turbulent Flow in a Tube From the analysis, the analytical solution give; Relates the heat transfer rate to the friction loss in tube flow Where, Heat transfer coefficient in term of the Nusselt No.  Pr ≈ 1.0 or Relation for turbulent heat transfer in smooth tube # from this analytical solution, shows that h higher than those observed in experiment Pr 2/3

  42. Turbulent Flow in a Tube Correct relation to used to calculate heat transfer in turbulent tube flow (The empirical relation) is: If wide temp. different are present in the flow also change in the fluid properties between the wall of the tube & the central flow used Note: All the empirical relation here apply to fully developed turbulent flow in tubes

  43. Turbulent Flow in a Tube More accurate although more complicated, the expression for fully developed turbulent flow in smooth tubeis; or All the properties using in this equation based on Tf 

  44. Turbulent Flow in a Tube For the entrance region (The flow is not developed), used:

  45. Example 6.1: Turbulent Heat Transfer in a Tube Air at 2 atm and 200 °C is heated as it flows through a tube with a diameter on 1 in (2.54 cm) at a velocity of 10 m/s. • Calculated the heat transfer per unit length of tube if a constant-heat-flux condition is maintained at the wall and the wall temp. is 20 °C above the air temp., all along the length of the tube. • How much would the bulk temp. increase over a 3m length of the tube?

  46. Example 6.2: Heating of Water in Laminar Tube Flow Water at 60 °C enters a tube of 1-in (2.54 cm) diameter at a mean flow velocity of 2 cm/s. Calculate the exit water temp. if the tube is 3.0 m long and the wall temp. is constant at 80 °C.

  47. Example 6.3: Heating of Air in Laminar Tube Flow for Constant Heat Flux Air at 1 atm and 27 °C enters a 5.0 mm diameter smooth tube with a velocity of 3.0 m/s. The length of the tube is 10 cm. A constant heat flux is imposed on the tube wall. • Calculate the heat transfer if the exit bulk temp. is 77 °C • Calculate the exit wall temp. and the value of h at exit

  48. Example 6.4: Heating of Air with Isothermal Tube Wall Air at 1 atm and 27 °C enters a 5.0 mm diameter smooth tube with a velocity of 3.0 m/s. The length of the tube is 10 cm. A constant wall temp. is imposed on the tube wall. • Calculate the heat transfer if the exit bulk temp. is 77 °C • Calculate the exit wall temp. and the value of h at exit

  49. Example 6.5: Heat Transfer in a Rough Tube A 2.0 cm diameter tube having a relative roughness of 0.001 is maintained at a constant wall temp. of 90 °C. Water enters the tube at 40 °C and leaves at 60 °C. if the entering velocity is 3 m/s, calculate the length of tube necessary to accomplish the heating.

  50. Liquid Metal Heat Transfer # Liquid metal  High heat transfer rate because of the higher thermal conductivities of liquid metal. # used in heat exchanger – so can compact design the HE. The relation for calculation of h in fully developed turbulent flow of liquid metal in smooth tubes with uniform heat flux at the wall: All properties at the bulk temp. The relation for calculation heat transfer to liquid metal in tubes with constant wall temp.:

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