Abstract
The experimental friction factor and Nusselt number data for laminar flow of viscous oil through a circular duct having integral axial corrugation roughness and fitted with twisted tapes with oblique teeth have been presented. Predictive friction factor and Nusselt number correlations have also been presented. The thermohydraulic performance has been evaluated. The major findings of this experimental investigation are that the twisted tapes with oblique teeth in combination with integral axial corrugation roughness perform significantly better than the individual enhancement technique acting alone for laminar flow through a circular duct up to a certain value of fin parameter.
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Abbreviations
- A:
-
Heat transfer area (m2)
- Ac:
-
Axial flow cross-sectional area = \( WD - \delta D \) (m2)
- Ao :
-
Plain duct flow cross-sectional area =W·D (m2)
- Cp:
-
Constant pressure specific heat (J/kg K)
- D:
-
Internal diameter of the plain duct (m)
- e:
-
Corrugation height (m)
- f :
-
Fully developed Fanning friction factor = \( \left( \frac{1}{2} \right)\left[ {\frac{{\Delta P^{\prime}}}{{\left( {\rho V_{0}^{2} } \right)}}} \right]\frac{D}{z} \), dimensionless
- g:
-
Gravitational acceleration (m/s2)
- Gr:
-
Grashof number = \( g\beta \rho^{2} D^{3}\Delta T_{w} /\mu^{2} \), dimensionless
- Gz:
-
Graetz number = \( \dot{m}C_{p} /kL \), dimensionless
- H:
-
Pitch for 180° rotation of twisted-tape (m)
- hz :
-
Axially local heat transfer coefficient (W/m2 K)
- k:
-
Fluid thermal conductivity (W/m K)
- L:
-
Axial length, length of the duct (m)
- \( \dot{m} \) :
-
Mass flow rate (kg/min)
- Num :
-
Axially averaged Nusselt number = \( \frac{1}{L}\int\limits_{0}^{L} {\frac{{h_{z} Ddz}}{k}} \), dimensionless
- \( \Delta P_{z} \) :
-
Pressure drop (mm)
- \( \Delta P^{\prime} \) :
-
Pressure drop (N/m2)
- P:
-
Wetted perimeter in the particular cross-section of the duct, corrugation pitch (P/e), dimensionless
- Pr:
-
Fluid Prandtl number = \( \mu C_{p} /k \), dimensionless
- Ra:
-
Rayleigh number = \( Gr \cdot \Pr \)
- Re:
-
Reynolds number based on plain duct diameter = \( \left( {\rho V_{0} D_{h} } \right)/\mu \), dimensionless
- T:
-
Temperature (K)
- \( t_{hl}^{*} \) :
-
Tooth horizontal length (m)
- \( t_{hl} = \frac{{t_{hl}^{*} }}{yD} \) :
-
Dimensionless
- ∆Tw :
-
Wall to fluid bulk temperature difference (K)
- Va :
-
Mean axial velocity = \( \dot{m}/\rho A_{c} \) (m/s)
- Vo :
-
Mean velocity based on plain duct diameter = \( \dot{m}/\rho A_{0} \) (m/s)
- X:
-
Prn, the value of n depends on the exponent of Pr in the correlation
- Y:
-
\( \left( {\frac{{\mu_{b} }}{{\mu_{w} }}} \right)^{ - 0.14} \times \frac{1}{5.172} \)
- y:
-
Twist ratio = H/D, dimensionless
- z:
-
Axial length, the distance between the measuring pressure taps (m)
- α:
-
Corrugation helix angle (°)
- β:
-
Coefficient of isobaric thermal expansion (K−1)
- δ:
-
Tape thickness (m)
- µ:
-
Fluid dynamic viscosity (kg/ms)
- ρ:
-
Density of the fluid (kg/m3)
- θ:
-
Twisted-tape tooth angle angle (°)
- b:
-
At bulk fluid temperature
- com:
-
Combined axial corrugation and twisted-tape
- hl:
-
Twisted-tape tooth horizontal length
- m:
-
Axially averaged
- oac, ott:
-
Only axial corrugation and only twisted-tape
- w:
-
At duct wall temperature, with
- z:
-
Local value
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Acknowledgments
The author gratefully acknowledges the generous financial support of the MHRD, DST, CSIR, Government of India for the current research.
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Appendix
Appendix
1.1 Uncertainty analysis
All the quantities that are measured to estimate the Nusselt number and the friction factor are subject to certain uncertainties due to errors in the measurement. These individual uncertainties as well as the combined effect of these are presented here. The analysis is carried out on the basis of the suggestion made by Kline and McClintock [50].
1.2 Analysis
First the analysis for the friction factor is presented. The analysis for the Nusselt number is presented after that.
1.2.1 Friction Factor
or,
The uncertainty in friction factor has been calculated from the above equations.
1.2.2 Nusselt number
or
where
The uncertainty in Nusselt number has been calculated from the above equations.
The accuracies of the measured quantities are given below in the tabular form:
Quantity | Accuracy | Quantity | Accuracy |
---|---|---|---|
ΔDh | 0.00002 m | ΔL | 0.001 m |
Δ\( \dot{m} \) | 1.667E−5 kg/s | Δh | 0.001 m |
ΔT | 0.025 °C | ΔV | 0.1 V |
ΔR | 0.0000 Ω |
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Pal, S., Saha, S.K. Experimental investigation of laminar flow of viscous oil through a circular tube having integral axial corrugation roughness and fitted with twisted tapes with oblique teeth. Heat Mass Transfer 51, 1189–1201 (2015). https://doi.org/10.1007/s00231-014-1489-8
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DOI: https://doi.org/10.1007/s00231-014-1489-8