Abstract
The subject of this chapter is the influence of flow field turbulence on heat transfer augmentation to both the turbulent and laminar boundary layers. Initially, the response of turbulence to the presence of a wall is reviewed as background to one of the key constraints in the interaction of turbulence to both turbulent and laminar boundary layers. Next, research on the influence of external turbulence to the flat plat turbulent boundary layer is discussed in terms of both the physics of the interaction of external turbulence with a developing turbulent boundary layer and the correlation of the resulting enhancement. A simple physics based eddy diffusivity model for the external turbulence is presented and predictive results using this model are presented and discussed. The influence of turbulence on laminar boundary layer heat transfer augmentation to stagnation region and other laminar regions is also reviewed. Initially, the influence of both the strain field and leading edge surface on the intensification of small scale turbulence and the blocking of relatively large scale turbulence is discussed. A physically based correlating method for stagnation region heat transfer augmentation is presented along with historical and alternate models. Heat transfer augmentation mechanisms in laminar regions with no intensification are also discussed and the simple physics based eddy diffusivity model for the turbulent boundary layer is extended to laminar flow prediction.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Abbreviations
- C:
-
turbine airfoil chord length (m2)
- Cf/2:
-
skin friction coefficient = τ/(ρU∞2/2)
- CP:
-
specific heat at constant pressure (J/kg/K)
- Cμ:
-
constant for k – ε model, Cμ = 0.09
- D:
-
pin, cylinder or leading edge diameter (m)
- E2(k1):
-
one dimensional energy spectrum function of v′, E2(k1) = U E2(f)/2/π (m3/s2)
- f:
-
frequency (1/s)
- fMIX:
-
blending function for mixing length and outer layer model
- fμ:
-
damping function for k – ε model
- h:
-
heat transfer coefficient (W/m2/K)
- HB:
-
the Hancock-Bradshaw correlating parameter, HB = \( {\left(\frac{{\mathrm{u}}^{\prime }}{\mathrm{U}}\right)}_{\mathrm{e}}\times 100/\left(\ \frac{{\mathrm{L}}_{\mathrm{e}}^{\mathrm{u}}}{\updelta_{.995}}+2.0\right) \)
- k:
-
thermal conductivity (W/m/K)
- k:
-
turbulent kinetic energy (m2/s2)
- K:
-
turbulent flow acceleration parameter, ν/U∞2 dU∞/dx
- k1:
-
wavenumber, k1 = 2πf/U (m−1)
- L:
-
macro-scale of turbulence (m)
- Lu:
-
energy scale, Lu = 1.5 |u’|3/ε (m)
- \( {\mathrm{L}}_{\mathrm{u}}^{\mathrm{e}} \) :
-
dissipation scale, Lu = 1.5 |u’|3/ε (m)
- l :
-
mixing length (m)
- Nu:
-
diameter Nusselt number, Nu = hD/k
- Pr:
-
Prandtl number, Pr = ν/α
- ReD:
-
diameter Reynolds number
- Reθ:
-
momentum thickness Reynolds number
- ReΔ2:
-
enthalpy thickness Reynolds number
- St:
-
Stanton number, h/ρ CP U∞
- St′:
-
Stanton prime, h/ρ CP u′
- t:
-
time (s)
- T+:
-
inner variable nondimensional temperature (K)
- TL + :
-
correlating parameter for turbulent boundary layer heat transfer
- TLR:
-
turbulence parameter for turbulent heat transfer, TLR = Tu (ReΔ2/1000)1/4(Δ2/Lu)1/3
- TRL:
-
turbulence parameter for stagnation heat transfer, TRL = Tu ReD5/12 (D/Lu)1/3
- Tu:
-
turbulence level, Tu = u′/U∞
- U:
-
streamwise velocity (m/s)
- U+:
-
velocity nondimensionalized on inner variables, U+ = U(Y)/uτ
- U:
-
streamwise velocity (m/s)
- uτ:
-
shear velocity, uτ = U.•(Cf/2)1/2 (m/s)
- u′:
-
rms streamwise fluctuation velocity (m/s)
- v′:
-
rms endwall normal fluctuation velocity (m/s)
- V:
-
normal velocity (m/s)
- W:
-
spanwise velocity (m/s)
- w′:
-
rms spanwise fluctuation velocity (m/s)
- x:
-
axial distance (m)
- y:
-
endwall normal distance (m)
- Y + :
-
dimensionless normal distance from wall in inner variables, Y+ = y uτ /ν
- α:
-
thermal diffusivity, m2/s
- δ , δ0.995:
-
boundary layer thickness, m
- δ2 , θ:
-
momentum thickness, m
- Δ2:
-
enthalpy thickness, m
- ε:
-
turbulent dissipation rate, m2/s3
- εM:
-
eddy diffusivity, m2/s
- κ:
-
mixing length model constant
- λ:
-
Taylor microscale, m
- λX:
-
streamwise integral scale of turbulence, m
- η, eta:
-
Kolmogorov length scale, η = (ν3/ε)1/4, m
- μ:
-
absolute viscosity, Pa s
- ν:
-
kinematic viscosity, m2/s
- ρ:
-
fluid density, mass per unit of volume, kg/m3
- τ:
-
shear stress, kg/m-s2
- ω:
-
specific dissipation, k – ω model, s−1
- ∞, e:
-
free-stream conditions, unaffected by wall
- 0:
-
low free-stream turbulence value
References
Ames FE (1994) Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence. NASA CR-4633
Ames FE (1996) Experimental study of vane heat transfer and film cooling at elevated levels of turbulence. NASA CR 198525
Ames FE (1997) The influence of large scale, high intensity turbulence on vane heat transfer. ASME J Turbomach 119:23
Ames FE, Dvorak LA (2006) Turbulent transport in pin fin arrays – experimental data and predictions. ASME J Turbomach 128:71–81
Ames FE, Moffat RJ (1990) Heat transfer with high intensity, large scale turbulence: the flat plate turbulent boundary layer and the cylindrical stagnation point, Report no. HMT-44, Thermosciences Division of Mechanical Engineering, Stanford University
Ames FE, Kwon O, Moffat RJ (1999) An algebraic model for high intensity large scale turbulence, ASME paper no. 99-GT-160
Ames FE, Wang C, Barbot PA (2003) Measurement and prediction of the influence of catalytic and dry low NOx combustor turbulence on vane surface heat transfer. ASME J Turbomach 125:210–220
Ames FE, Argenziano M, Wang C (2004) Measurement and prediction of heat transfer distributions on an aft loaded vane subjected to the influence of catalytic and dry low NOx combustor turbulence. ASME J Turbomachi 126:139–149
Ames FE, Dvorak LA, Morrow MJ (2005) Turbulent augmentation of internal convection off pins in staggered pin fin arrays. ASME J Turbomach 127:183–190
Bae S, Lele SK, Sung HG (2002) The influence of inflow disturbances on stagnation region heat transfer. ASME J Heat Transfer 122:258–265
Barrett MJ, Hollingsworth DK (2003a) Heat transfer in turbulent boundary layers subjected to free-stream turbulence—part I: experimental results. J Turbomach 125(2):232–241
Barrett MJ, Hollingsworth DK (2003b) Heat transfer in turbulent boundary layers subjected to free-stream turbulence—part II: analysis and correlation. J Turbomach 125(2):242–251
Becko Y (1975) Heat transfer analysis along the blades of a gas turbine stator by thermal and kinematic boundary layer theory, ASME paper no. 75-GT-15
Blair MF (1983a) Influence of free-stream turbulence on turbulent boundary layer heat transfer and mean profile development, part I-experimental data. J Heat Transf 105:33
Blair MF (1983b) Influence of free-stream turbulence on turbulent boundary layer heat transfer and mean profile development, part II-analysis of results. J Heat Transf 105:41
Blair MF, Werle MJ (1980) The influence of free-stream turbulence on the zero-pressure gradient fully turbulent boundary layer, UTRC Report R-80-914388-12
Boyle RJ, Ameri AA (2015) Effects of turbulence intensity and scale on turbine blade heat transfer, ASME paper no. GT2015–43597
Boyle RJ, Giel PW, Ames FE (2004) Predictions for the effects of freestream turbulence on turbine blade heat transfer, ASME paper no. GT-2004-54332
Britter RE, Hunt JCR, Mumford JC (1979) The distortion of turbulence by a circular cylinder. J Fluid Mech 92(2):269
Brown A, Burton RC (1978) The effects of free-stream turbulence intensity and velocity distribution on heat transfer to curved surfaces. ASME J Eng Power 100:159–165
Charnay G, Mathieu J, Comte-Bellot G (1976) Response of the turbulent boundary layer to random fluctuations in the external stream. Phys Fluids 19(9):1261
Chowdhury NHK, Ames FE (2013) The response of high intensity turbulence in the presence of large stagnation regions, ASME paper no. GT2013–95055
Dullenkopf K, Mayle RE (1995) An account of free-stream turbulence length scale on laminar heat transfer. ASME J Turbomach 117:401–406
Dunham J (1972) Predictions of boundary layer transition on turbomachinery blades (Predictions of boundary layer transition on turbomachine blades). AGARD-AG-164, pp 55–71
Durbin PA (1995) Separated flow computations with the k-epsilon-v-squared model. AIAA J 33(4):659–664
Forest AE (1977) Engineering predictions of transitional boundary layers. In AGARD Laminar-Turbulent Transition 19 p (SEE N78-14316 05-34)
Gandaparavu P, Ames FE (2013) The influence of leading edge diameter on stagnation region heat transfer augmentation including effects of turbulence level, scale, and Reynolds number. ASME J Turbomach 135:011008-1-8
Gifford AR, Diller TE, Vlachos PP (2011) The physical mechanism of heat transfer augmentation in stagnation flow subject to freestream turbulence. ASME J Heat Transfer 133:021901-1-11
Hancock PE, Bradshaw P (1983) The effect of free stream turbulence on turbulent boundary layers. J Fluids Eng 105:284
Hancock PE, Bradshaw P (1989) Turbulence structure of a boundary layer beneath a turbulent free stream. J Fluid Mech 205:45
Hollingsworth DK, Bourgogne HA (1995) The development of a turbulent boundary layer in high free-stream turbulence produced by a two-stream mixing layer. Exp Thermal Fluid Sci 11 (2):210–222
Huffman GD, Zimmerman DR, Bennett WA (1972) The effect of free stream turbulence level on the flow and heat transfer in the entrance region of an annulus. Int J Heat Mass Transf 20:763
Hunt JCR (1973) A theory of turbulent flow round two-dimensional bluff bodies. J Fluid Mech 61(part 4):625
Hunt JCR, Graham JMR (1978) Free-stream turbulence near plane boundaries. J Fluid Mech 84:209
Hylton LD, Mihelc MS, Turner ER, Nealy DA, York RE (1983) Analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes. National Aeronautics and Space Administration, NASA Lewis Research Center, Cleveland
Kestin J (1966) The effect of free-stream turbulence on heat transfer rate. In: Irvine TF, Harnett JP (eds) Advances in heat transfer, 3rd edn. Academic, London
Kestin J, Wood RT (1971) The influence of turbulence on mass transfer from cylinders. J Heat Transf 93(4):321
Kingery JA, Ames FE (2016) Stagnation region heat transfer augmentation at very high turbulence levels. ASME J Turbomach 138(8):081005. https://doi.org/10.1115/1.4032677. (10 pages)
Kwon O, Ames FE (1996) A velocity and length scale approach to k-ε modeling. ASME J Heat Transf 118: 857.
Lander RD (1969) Evaluation of the effect of free stream turbulence on the heat transfer to turbine airfoil (No. PWA-3713). Pratt and Whitney Aircraft Group East Hartford
Lowery GW, Vachon RI (1975) The effect of turbulence on heat transfer from heated cylinders. Int J Heat Mass Transf 18:1229
Maciejewski PK, Moffat RJ (1989) Heat transfer with very high free-stream turbulence, Report HMT-42, Deptartment of Mechanical Engineering, Stanford University
Maciejewski PK, Moffat RJ (1992) Heat transfer with very high free-stream turbulence: part I-experimental data and part II-analysis of results. ASME J Heat Transfer 114:847
MacMullin R, Elrod W, Rivir R (1989) Free-stream turbulence from a circular wall jet on a flat plate heat transfer and boundary layer flow. J Turbomach 111(1):78–86
Mayle RE (1991) The role of laminar-turbulent transition in gas turbine engines, 1991 ASME international gas turbine institute scholar award paper. J Turbomach 113:509–537
Medic GG, Durbin PA (2002) Toward improved prediction of heat transfer on turbine blades. ASME J Turbomach 124(2):187–192. https://doi.org/10.1115/1.1458020.
Mehendale AB, Han JC, Ou S (1991) Influence of high mainstream turbulence on leading edge heat transfer. ASME J Heat Transfer 113:843–850
Miyazaki HH, Sparrow EM (1977) Analysis of effects of free-stream turbulence on heat transfer and skin friction. ASME J Heat Transfer 99(4):614–619. https://doi.org/10.1115/1.3450751.
Nealy DA, Mihelc MS, Hylton LD, Gladden HJ (1984) Measurements of heat transfer distribution over the surfaces of highly loaded turbine nozzle guide vanes. J Eng Gas Turbines Power 106:149–158
Nix AC, Diller TE (2009) Experiments on the physical mechanism of heat transfer augmentation by freestream turbulence at a cylinder stagnation point. ASME J Turbomach 131(2):021015-021015-7. https://doi.org/10.1115/1.2950079
Nix AC, Diller TE, Ng WF (2007) Experimental measurements and modeling of the effects of large-scale freestream turbulence on heat transfer. ASME J Turbomach 129:542–550
Oo AN, Ching CY (2002) Stagnation line heat transfer augmentation due to freestream vortical structures and vorticity. ASME J Heat Transfer 124:583–587
Rigby DL, Van Fossen GJ (1991) Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity. In: AIAA-91-1739, AIAA 22nd fluid dynamics, plasma dynamics and lasers conference, Honolulu
Sadeh WZ, Sullivan PP (1980) Turbulence amplification in flow about an airfoil. In: ASME 1980 international gas turbine conference and products show, ASME paper no. 80-GT-111, pp V01BT02A017-V01BT02A017
Sahm MK, Moffat RJ (1992) Turbulent boundary layers with high turbulence: experimental heat transfer and structure on flat and convex walls, Report no. HMT-45, Deptartment of Mechanical Engineering, Stanford University
Sanitjai S, Goldstein RJ (2001) Effect of free stream turbulence on local mass transfer from a circular cylinder. Int J Heat Mass Transf 44(15):2863–2875
Schmidt RC, Patankar SV (1988) Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades. PhD thesis, Final contractor report, NASA CR 4145
Smith MC, Kuethe AM (1966) Effects of turbulence on laminar skin friction and heat transfer. Phys Fluids 9(12):2337
Thole KA, Bogard DG (1995) Enhanced heat transfer and skin friction due to high freestream turbulence. ASME J Turbomach 117:418
Thomas NH, Hancock PE (1977) Grid turbulence near a moving wall. J Fluid Mech 82(Part 3):481
Turner AB (1971) Local heat transfer measurements on a gas turbine blade. J Mech Eng Sci 13(1):1–12
Uzkan T, Reynolds WC (1967) A shear-free turbulent boundary layer. J Fluid Mech 28:803
Van Fossen GJ, Bunker RS (2001) Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor. ASME J Turbomach 123:140–146
Van Fossen GJ, Bunker RS (2002) Augmentation of stagnation region heat transfer due to turbulence from an advanced dual-annular combustor. In: ASME Turbo Expo 2002: power for land, sea, and air, ASME paper no. GT2002–30184, pp 199–206
Van Fossen GJ, Simoneau RJ, Ching CY (1995) Influence of turbulence parameters, Reynolds number, and body shape on stagnation region heat transfer, ASME. J Heat Transf 117:597–603
Varty J, Ames FE (2016) Experimental heat transfer distributions over an aft loaded vane with a large leading edge at very high turbulence levels, ASME paper no. IMECE2016-67029
Wissink JG, Rodi W (2011) Direct numerical simulation of heat transfer from the stagnation region of a heated cylinder affected by an impinging wake. J Fluid Mech 669:64–89
Zapp GM (1950) The effect of turbulence on local heat transfer coefficients around a cylinder normal to an air stream. Master’s thesis, Oregon State College
Zukauskas A, Ziugzda J (1985) Heat transfer of a cylinder in crossflow. Hemisphere Publishing Corporation, Washington, DC
Author information
Authors and Affiliations
Corresponding author
Section Editor information
Rights and permissions
Copyright information
© 2018 Springer International Publishing AG, part of Springer Nature
About this entry
Cite this entry
Ames, F.E. (2018). Turbulence Effects on Convective Heat Transfer. In: Handbook of Thermal Science and Engineering. Springer, Cham. https://doi.org/10.1007/978-3-319-26695-4_17
Download citation
DOI: https://doi.org/10.1007/978-3-319-26695-4_17
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-26694-7
Online ISBN: 978-3-319-26695-4
eBook Packages: EngineeringReference Module Computer Science and Engineering