NUMERICAL STUDY OF HEAT TRANSFER SYSTEM WITH STAGGERED ARRAY OF VERTICAL FLAT PLATES USED AT LOW REYNOLDS NUMBER

The boundary layer development and convective heat transfer on transonic turbine nozzle vanes are investigated using a compressible Navier–Stokes code with three low-Reynolds-number k–ε models. The mean-flow and turbulence transport equations are integrated by a four-stage Runge–Kutta scheme. Numerical predictions are compared with the experimental data acquired at Allison Engine Company. An assessment of the performance of various turbulence models is carried out. The two modes of transition, bypass transition and separation-induced transition, are studied comparatively. Effects of blade surface pressure gradients, free-stream turbulence level, and Reynolds number on the blade boundary layer development, particularly transition onset, are examined. Predictions from a parabolic boundary layer code are included for comparison with those from the elliptic Navier–Stokes code. The present study indicates that the turbine external heat transfer, under real engine conditions, can be predicted well by the Navier–Stokes procedure with the low-Reynolds-number k–ε models employed.

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A numerical study of low reynolds number 2-dimensional convective adjustment

Geophysical & Astrophysical Fluid Dynamics ◽

10.1080/03091929408203635 ◽

1994 ◽

Vol 74 (1-4) ◽

pp. 123-134 ◽

Cited By ~ 5

Author(s):

Charles A. Lin ◽

David Dietrich

Keyword(s):

Reynolds Number ◽

Numerical Study ◽

Low Reynolds Number ◽

Convective Adjustment ◽

Low Reynolds

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Numerical Simulations of Resonant Heat Transfer Augmentation at Low Reynolds Numbers

10.1115/imece2001/htd-24100 ◽

2001 ◽

Author(s):

Miles Greiner ◽

Paul F. Fischer ◽

Henry Tufo

Keyword(s):

Heat Transfer ◽

Reynolds Number ◽

Natural Frequency ◽

Flow Rate ◽

Low Reynolds Number ◽

Reynolds Numbers ◽

Spectral Element ◽

Pumping Power ◽

Number Systems ◽

Low Reynolds

Abstract The effect of flow rate modulation on low Reynolds number heat transfer enhancement in a transversely grooved passage was numerically simulated using a two-dimensional spectral element technique. Simulations were performed at subcritical Reynolds numbers of Rem = 133 and 267, with 20% and 40% flow rate oscillations. The net pumping power required to modulate the flow was minimized as the forcing frequency approached the predicted natural frequency. However, mixing and heat transfer levels both increased as the natural frequency was approached. Oscillatory forcing in a grooved passage requires two orders of magnitude less pumping power than flat passage systems for the same heat transfer level. Hydrodynamic resonance appears to be an effective method of increasing heat transfer in low Reynolds number systems where pumping power is at a premium, such as micro heat transfer applications.

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Numerical Study on Low Reynolds Number Flows Over an Aerofoil

Journal of Applied Mechanical Engineering ◽

10.4172/2168-9873.1000131 ◽

2013 ◽

Vol 02 (05) ◽

Cited By ~ 3

Author(s):

Ilyas Karasu M. Serdar Genc

Keyword(s):

Reynolds Number ◽

Numerical Study ◽

Low Reynolds Number ◽

Low Reynolds Number Flows ◽

Low Reynolds ◽

Reynolds Number Flows

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Numerical Study of Deteriorated Convection Heat Transfer of Supercritical Fluid Flowing Through Vertical Mini Tube at Relatively Low Reynolds Numbers

Volume 6A: Thermal-Hydraulics and Safety Analyses ◽

10.1115/icone26-81012 ◽

2018 ◽

Author(s):

Chen-Ru Zhao ◽

Zhen Zhang ◽

Qian-Feng Liu ◽

Han-Liang Bo ◽

Pei-Xue Jiang

Keyword(s):

Heat Transfer ◽

Heat Flux ◽

Reynolds Number ◽

Low Reynolds Number ◽

Convection Heat Transfer ◽

Turbulence Models ◽

Convection Heat ◽

Flow Acceleration ◽

Heat Transfer Deterioration ◽

Low Reynolds

Numerical investigations are performed on the convection heat transfer of supercritical pressure fluid flowing through vertical mini tube with inner diameter of 0.27 mm and inlet Reynolds number of 1900 under various heat fluxes conditions using low Reynolds number k-ε turbulence models due to LB (Lam and Bremhorst), LS (Launder and Sharma) and V2F (v2-f). The predictions are compared with the corresponding experimentally measured values. The prediction ability of various low Reynolds number k-ε turbulence models under deteriorated heat transfer conditions induced by combinations of buoyancy and flow acceleration effects are evaluated. Results show that all the three models give fairly good predictions of local wall temperature variations in conditions with relatively high inlet Reynolds number. For cases with relatively low inlet Reynolds number, V2F model is able to capture the general trends of deteriorated heat transfer when the heat flux is relatively low. However, the LS and V2F models exaggerate the flow acceleration effect when the heat flux increases, while the LB model produces qualitative predictions, but further improvements are still needed for quantitative prediction. Based on the detailed flow and heat transfer information generated by simulation, a better understanding of the mechanism of heat transfer deterioration is obtained. Results show that the redistribution of flow field induced by the buoyancy and flow acceleration effects are main factors leading to the heat transfer deterioration.

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