1 / 173

CHAPTER 2 CONVECTION

HEAT TRANSFER. CHAPTER 2 CONVECTION. Dr. R. VELRAJ, PROFESSOR ANNA UNIVERSITY CHENNAI. IN THIS SESSION. 1. Introduction to Convection 2. Boundary Layer Concepts. CHAPTER 2 (CONVECTION) – SESSION 1. GOVERNING LAW. Newton’s Law of Cooling Q = h A ( T w – T ∞ ).

hilda-downs
Download Presentation

CHAPTER 2 CONVECTION

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. HEAT TRANSFER CHAPTER 2CONVECTION Dr. R. VELRAJ, PROFESSOR ANNA UNIVERSITY CHENNAI

  2. IN THIS SESSION 1. Introduction to Convection2. Boundary Layer Concepts CHAPTER 2 (CONVECTION) – SESSION 1

  3. GOVERNING LAW Newton’s Law of CoolingQ = h A (Tw – T∞) h – convective heat transfer coefficient A – surface area over which convection occurs • (Tw – T∞) – temperature potential difference Convection 1

  4. CONCEPT OF BOUNDARY LAYER y TURBULENT REGION LAMINAR REGION TRANSITION x Flow Regimes on a flat plate u∞ u u∞ u FLAT PLATE u = 0 at y = 0 u = u∞ at y = δ Convection 2

  5. FLOW REGIMES ON A FLAT PLATE y Reynolds’ no. x LAMINAR BOUNDARY LAYER Laminar Region (Re < 5 x 105) u∞ u FLAT PLATE τ - Shear stress µ - Dynamic viscosity (proportionality constant) Convection 3

  6. REYNOLDS’ NUMBER Laminar Region ρ Density, kg / m3 u∞ Free Stream Velocity, m / s x Distance from leading edge, m µ Dynamic viscosity, kg / m-s Re < 5 x 105 FLOW OVER FLAT PLATE Re < 2300 FLOW THROUGH PIPE Convection 4

  7. FLOW REGIMES ON A FLAT PLATE TRANSITION Transition Region FLAT PLATE 5 x 105< Re < 106 FLOW OVER FLAT PLATE 2000 < Re < 4000 FLOW THROUGH PIPE Convection 5

  8. FLOW REGIMES ON A FLAT PLATE y x Turbulent Region TURBULENT BOUNDARY LAYER TURBULENT CORE u∞ BUFFER ZONE u LAMINAR SUB LAYER FLAT PLATE Convection 6

  9. FLOW THROUGH TUBE y BOUNDARY LAYER UNIFORM INLET FLOW x Flow Development FULLY DEVELOPED FLOW STARTING LENGTH Convection 7

  10. THERMAL BOUNDARY LAYER y T∞ x TEMPERATURE PROFILE δt TW FLAT PLATE Convection 8

  11. Dimensional Analysis • Reduces the number of independent variables in a problem. • Experimental data can be conveniently presented in terms of dimensionless numbers. • Buckingham’s Pi theorem is used a rule of thumb for determining the dimensionless groups that can be obtained from a set of variables. Convection 9

  12. Buckingham’s Pi theorem Number of independent dimensionless groups that can be formed from a set of ‘m’ variables having ‘n’ basic dimensions is (m – n) Convection 10

  13. QUESTIONS FOR THIS SESSION What is Newton’s Law of Cooling ? Draw the boundary layer for a flow over a flat plate indicating the velocity distribution in the laminar and turbulent flow region. Draw the boundary layer for flow over through tube. Define Buckingham’s π theorem End of Session

  14. Dimensional Analysis • Reduces the number of independent variables in a problem. • Experimental data can be conveniently presented in terms of dimensionless numbers. • Buckingham’s Pi theorem is used a rule of thumb for determining the dimensionless groups that can be obtained from a set of variables. Convection 9

  15. Buckingham’s Pi theorem Number of independent dimensionless groups that can be formed from a set of ‘m’ variables having ‘n’ basic dimensions is (m – n) Convection 10

  16. Dimensional Analysis for Forced Convection Consider a case of fluid flowing across a heated tube Convection 11

  17. Dimensional Analysis for Forced Convection • There are 7 (m) variables and 4 (n) basic dimensions. • 3 (m-n) dimensionless parameters symbolized as π1 ,π2, π3can be formed. • Each dimensionless parameter will be formed by combining a core group of ‘n’ variables with one of the remaining variables not in the core. • The core group will include variables with all of the basic dimensions Convection 12

  18. Dimensional Analysis for Forced Convection Choosing D, ρ, µ and k as the core (arbitrarily), the groups formed is represented as: π1 = DaρbµckdU π2 = DeρfµgkhCp π3 = Djρlµmknh Since these groups are to be dimensionless, the variables are raised to certain exponents (a, b, c,….) Convection 13

  19. Dimensional Analysis for Forced Convection Starting with π1 Equating the sum of exponents of each basic dimension to 0, we get equations for: M 0 = b + c + d L 0 = a – 3b + d + 1 + e T 0 = -d t 0 = -c -3d -1 Convection 14

  20. Dimensional Analysis for Forced Convection Solving these equations, we get: d = 0, c = -1, b = 1, a = 1 giving Similarly for π2 Convection 15

  21. Dimensional Analysis for Forced Convection Equating the sum of exponents M 0 = f + g + I L 0 = e – 3f – g + i + 2 T 0 = -i – 1 t 0 = -g – 3i -2 Solving, we get e = 0, f = 0, g = 1, i = 1 giving Convection 16

  22. Dimensional Analysis for Forced Convection By following a similar procedure, we can obtain The relationship between dimensionless groups can be expressed as F(π1, π2, π3) = 0. Thus, Convection 17

  23. Dimensional Analysis for Forced Convection • Influence of selecting the core variables • Choosing different core variables leads to different dimensionless parameters. • If D, ρ, µ, Cp were chosen, then the π groups obtained would be Re, Pr and St. • St is Stanton number, a non dimensional form of heat transfer coefficient. Convection 18

  24. Dimensional Analysis for FreeConvection Free Convection on a Vertical Plate g T∞ (FLUID) TS (SURFACE) L FLUID PROPERTIES ρ,µ, CP, k, βg Convection 19

  25. Dimensional Analysis for FreeConvection Free Convection on a Vertical Plate In free convection, the variable U is replaced by the variables ΔT, β and g. Convection 20

  26. Dimensional Analysis for FreeConvection Convection 21

  27. Dimensional Analysis for Free Convection Choosing L, ρ, µ and k as the core (arbitrarily), the groups formed is represented as: π1 = LaρbµckdΔT π2 = Leρfµikjβg π3 = LlρmµnkoCp π4 = Lpρqµrksh Convection 22

  28. Dimensional Analysis for Free Convection Following the procedure outlined in last section, we get: π1 = (L2ρ2 k ΔT) / µ2 π2 = (Lµβg) / k π3 = (µCp) / k = Pr (Prandtl number) π4 = (hL) / k = Nu (Nusselt number) Grashof Number Convection 23

  29. Dimensional Analysis FORCEDCONVECTION FREECONVECTION Convection 24

  30. PRANDTL NUMBER Multiplying with ρ in the numerator and denominator, Prair = 0.7 Prwater = 4.5 Prliquid Na = 0.011 Convection 25

  31. PRANDTL NUMBER Pr << 1 Pr >> 1 δh δt δt δh Pr = 1 δt=δh δh = Hydrodynamic thickness δt = Thermal Boundary layer thickness Convection 26

  32. QUESTIONS FOR THIS SESSION What are the dimensionless numbers involved in forced convection and free convection ? Define Prandtl number. List the advantages of using liquid metal as heat transfer fluid. Draw the hydrodynamic and thermal boundary layer (in the same plane) for Pr << 1, Pr >> 1 & Pr = 1. End of Session

  33. What is … Continuity Equation Momentum Equation Energy Equation Convection 27

  34. Laminar – Momentum Equation –Flat Plate y u∞ x dy dx FLAT PLATE Convection 28

  35. Laminar Boundary Layer on a Flat Plate Momentum Equation Assumptions Fluid is incompressible Flow is steady No pressure variations in the direction perpendicular to the plate Viscosity is constant Viscous-shear forces in ‘y’ direction are negligible. Convection 29

  36. Continuity Equation Velocity y x u - Velocity in x direction v - Velocity in y direction Convection 30

  37. Continuity Equation – Laminar – Flat Plate Mass flow Convection 31

  38. Continuity Equation Mass balance Mass balance on the element yields: Or Mass Continuity Equation Convection 32

  39. Momentum Equation – Laminar – Flat Plate Pressure Forces y x p - Pressure Convection 33

  40. Momentum Equation – Laminar – Flat Plate Shear Stresses y x µ - Dynamic viscosity u - Velocity in x direction v - Velocity in y direction Convection 34

  41. Momentum Equation – Laminar – Flat Plate Newton’s 2nd Law • Momentum flux in x direction is the product of mass flow through a particular side of control volume and x component of velocity at that point Convection 35

  42. Momentum Equation – Laminar – Flat Plate Momentum flux Convection 36

  43. Momentum Equation – Laminar – Flat Plate Momentum and Force Analysis Net pressure force Net Viscous-Shear force Convection 37

  44. Momentum Equation – Laminar – Flat Plate Equating the sum of viscous-shear and pressure forces to the net momentum transfer in x direction, making use of continuity relation and neglecting second order differentials: Convection 38

  45. Energy Equation – Assumptions Incompressible steady flow Constant viscosity, thermal conductivity and specific heat. Negligible heat conduction in the direction of flow (x direction). y x u∞ dy dx FLAT PLATE Convection 39

  46. Energy Equation – Laminar – Flat Plate y dy x dx Energy convected in (left face + bottom face) + heat conducted in bottom face + net viscous work done on element Energy convected out in (right face + top face) + heat conducted out from top face Convection 40

  47. Energy Equation – Laminar – Flat Plate Energy Convected y x u - Velocity in x direction v - Velocity in y direction Convection 41

  48. Energy Equation – Laminar – Flat Plate Heat Conducted y x Net Viscous Work u - Velocity in x direction v - Velocity in y direction Convection 42

  49. Energy Equation – Laminar – Flat Plate Net Viscous Work u - Velocity in x direction v - Velocity in y direction Convection 43

  50. Energy Equation – Laminar – Flat Plate Writing energy balance corresponding to the quantities shown in figure, assuming unit depth in the z direction, and neglecting second-order differentials: Convection 44

More Related