Abstract
Turbulent heat and mass transfer of a rotating disk for Prandtl and Schmidt numbers much larger than unity was modeled using an integral method validated against empirical equations of different authors for Sherwood numbers. As shown, decrease in relative thickness of thermal/diffusion boundary layers with increasing local radii entails additional increase of the exponent at the Reynolds number in expressions for Nusselt and Sherwood numbers in comparison with air flows.
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Abbreviations
- a :
-
Thermal diffusivity (m2/s)
- b :
-
Outer radius of disk (m)
- c f/2:
-
Friction coefficient \( \left( { =\tau_{\text{w}} /\left( {\rho V_{*}^{2} } \right)} \right) \)
- C :
-
Concentration (mol/m3)
- c p :
-
Isobaric specific heat (J/(kg K))
- D m :
-
Diffusion coefficient (m2/s)
- h m :
-
Mass transfer coefficient (m/s)
- h m,av :
-
Average mass transfer coefficient (m/s) \( ( { ={\frac{2}{{b^{2} }}}\int\nolimits_{0}^{b} {h_{\text{m}} rdr} }) \)
- k :
-
Thermal conductivity (W/(m K))
- K 1, K 2 :
- n R :
- n * :
-
Exponent in Eq. 3
- n, n T :
- Nu :
-
Nusselt number \( \left( { =q_{\text{w}} r/[k\Updelta T]} \right) \)
- Nu av :
-
Average Nusselt number \( \left( { =q_{{{\text{w}},{\text{av}}}} b/[k\Updelta T_{\text{av}} ]} \right) \)
- Pr :
-
Prandtl number (=ν/a)
- q w :
-
Local heat flux at the wall (W/m2)
- q w,av :
-
Average heat flux at the wall (W/m2) \(( {={{\int\nolimits_{0}^{b} {q_{\text{w}} rdr} } \mathord{\left/ {\vphantom {{\int\nolimits_{0}^{b} {q_{\text{w}} rdr} } {\int\nolimits_{0}^{b} {rdr} }}} \right. \kern-\nulldelimiterspace} {\int\nolimits_{0}^{b} {rdr} }}}) \)
- r, φ, z :
-
Radial, tangential and axial coordinate (m)
- Re ω :
-
Local Reynolds number (=ωr 2/ν)
- Re φ :
-
Reynolds number (=ωb 2/ν)
- Re V* :
-
Reynolds number \( \left( { ={{V_{*} \delta } \mathord{\left/ {\vphantom {{V_{*} \delta } \nu }} \right. \kern-\nulldelimiterspace} \nu }} \right) \)
- Sc :
-
Schmidt number (=ν/D m)
- Sh :
-
Sherwood number \( \left( { =h_{\text{m}} r/D_{\text{m}} } \right) \)
- Sh av :
-
Average Sherwood number \( \left( { =h_{\text{m,av}} b/D_{\text{m}} } \right) \)
- St :
-
Stanton number \( \left( { =q_{\text{w}} /\rho c_{p} V_{*} \Updelta T} \right) \)
- T :
-
Temperature (K)
- T + :
-
Temperature in wall coordinates (K) \( \left( { =(T_{\text{w}} - T){{\uprho}}c_{\rm p} V_{\tau } /q_{\text{w}} } \right) \)
- tanφ:
-
Tangent of the flow swirl angle \( \left( { =v_{\rm r} /(\omega \, r - v_{\varphi } )} \right) \)
- v r :
-
Radial, tangential and axial
- v φ, v z :
-
Velocity components (m/s)
- V :
-
Total velocity (m/s) \(( { =\left[ {{\text{v}}_{\rm r}^{2} + ({\text{v}}_{\varphi } - \omega \, r)^{2} } \right]^{1/2} }) \)
- V + :
-
Velocity in wall coordinates (m/s) \( \left( { =V/V_{\tau } } \right) \)
- V τ :
-
Friction velocity (m/s) (=(τw/ρ)1/2)
- V * :
-
Characteristic velocity (m/s) \( \left( { =\omega \, r(1 + {{\upalpha}}^{2} )^{1/2} } \right) \)
- z + :
-
Wall coordinate \( \left( { =zV_{\tau } /{{\upnu}}} \right) \)
- α:
-
Value of tanφ at z = 0
- δ:
-
Boundary layer thickness (m)
- δT :
-
Thermal/diffusion boundary layer thickness (m)
- Δ:
-
Dimensionless ratio (= δ T /δ)
- \( \Updelta T \) :
-
Temperature difference (K) \(( { = T_{w} - T_{\infty } }) \)
- \( \Updelta T_{\text{av}} \) :
-
Average temperature difference (K) \( ( { = {{\int\nolimits_{0}^{b} {(T{}_{w} - T_{\infty } )rdr} } \mathord{\left/ {\vphantom {{\int\nolimits_{0}^{b} {(T{}_{w} - T_{\infty } )rdr} } {\int\nolimits_{0}^{b} {rdr} }}} \right. \kern-\nulldelimiterspace} {\int\nolimits_{0}^{b} {rdr} }}}) \)
- Θ:
-
Dimensionless temperature \( \left( { = (T - T_{\text{w}} )/(T_{\infty } - T_{\text{w}} )} \right) \)
- μ:
-
Dynamic viscosity (Pa s)
- ν:
-
Kinematic viscosity (m2/s)
- ξ:
-
Dimensionless coordinate (= z/δ)
- ξ T :
-
Dimensionless coordinate (= z/δ T )
- ρ:
-
Density (kg/m3)
- τwr :
-
Radial shear stress at the wall (Pa) \( ( = \mu (d{\text{v}}_{\rm r} /dz)_{z = 0} ) \)
- τwφ :
-
Tangential shear stress at the wall (Pa) \( \left( { = \mu (d{\text{v}}_{\varphi } /dz)_{z = 0} } \right) \)
- τw :
-
Total wall shear stress (Pa) \( ( { = (\tau_{wr}^{2} + \tau_{w\varphi }^{2} )^{1/2} }) \)
- ω:
-
Angular speed of the disk (1/s)
- av:
-
Average value
- w:
-
Wall (z = 0)
- T:
-
Thermal boundary layer
- 1:
-
Boundary of a sub-layer
- ∞:
-
Infinity
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Acknowledgments
The research results presented in this work were obtained in part due to the gratefully acknowledged support of the Research Fellowship of the Alexander von Humboldt Foundation taken by the author at TU Dresden, Germany.
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Shevchuk, I.V. Turbulent heat and mass transfer over a rotating disk for the Prandtl or Schmidt numbers much larger than unity: an integral method. Heat Mass Transfer 45, 1313–1321 (2009). https://doi.org/10.1007/s00231-009-0505-x
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DOI: https://doi.org/10.1007/s00231-009-0505-x