Abstract
Computational investigations on the rib turbulated flow inside a convergent and divergent rectangular channel with square ribs of different rib heights and different Reynolds numbers (Re=20,000, 40,000 and 60,000). The ribs were arranged in a staggered fashion between the upper and lower surfaces of the test section. Computational investigations are carried out using computational fluid dynamic software ANSYS Fluent 14.0. Suitable solver settings like turbulence models were identified from the literature and the boundary conditions for the simulations on a solution of independent grid. Computations were carried out for both convergent and divergent channels with 0 (smooth duct), 1.5, 3, 6, 9 and 12 mm rib heights, to identify the ribbed channel with optimal performance, assessed using a thermo hydraulic performance parameter. The convergent and divergent rectangular channels show higher Nu values than the standard correlation values.
References
1 Webb BW, Ramadhyani S. Conjugate heat transfer in a channel with staggered ribs. Int J Heat Mass Transfer 1985;28:1679–87.10.1016/0017-9310(85)90142-5Suche in Google Scholar
2 Becker BR, Becker CS. The flow field and heat transfer near a turbulator. Int Commun Heat Mass Transfer 1990;17:455–64.10.1016/0735-1933(90)90064-QSuche in Google Scholar
3 Luy CD, Chaeng CH, Huang WH. Forced convection in parallel-plate channels with a series of fins mounted on the wall. Appl Energy 1991;39:127–44.10.1016/0306-2619(91)90026-TSuche in Google Scholar
4 Naimi M, Gessner FB. Calculation of fully developed turbulent flow in rectangular ducts with two opposite roughened walls. Int J Heat Fluid Flow 1997;18:471–81.10.1016/S0142-727X(97)80005-7Suche in Google Scholar
5 Kim KY, Kim SS. Shape optimization of rib-roughened surface to enhance turbulent heat transfer. Int J Heat Mass Transfer 2002;45:2719–27.10.1016/S0017-9310(01)00358-1Suche in Google Scholar
6 Promvonge P, Sripattanapipat S, Tamna S, Kwankaomeng S, Thianpong C. Numerical investigation of laminar heat transfer in a square channel with 45° inclined baffles. Int Commun Heat Mass Transfer 2010;37:170–7.10.1016/j.icheatmasstransfer.2009.09.010Suche in Google Scholar
7 Wang Y, Hou M, Deng X, Li L, Huang C, Guang H, et al. Configuration optimization of regularly spaced short-length twisted tape in a circular tube to enhance turbulent heat transfer using CFD modelling. Appl Therm Eng 2011;31:1141–9.10.1016/j.applthermaleng.2010.12.009Suche in Google Scholar
8 Tang XY, Zhu DS. Flow structure and heat transfer in a narrow rectangular channel with different discrete rib arrays. Chem Eng Process 2013;69:1–14.10.1016/j.cep.2013.01.005Suche in Google Scholar
9 Wang LB, Wang QW, He YL, Tao WQ. Experimental and numerical study of developing turbulent flow and heat transfer in convergent/divergent square ducts. Heat Mass Transfer 2002;38:399–408.10.1007/s002310100209Suche in Google Scholar
10 Yadav AS, Bhagoria JL. A numerical investigation of square sectioned transverse rib roughened solar air heater. Int J Therm Sci 2014;70:111–31.10.1016/j.ijthermalsci.2014.01.008Suche in Google Scholar
11 Sivakumar K, Kulasekharan N, Natarajan E. Experimental study of developing turbulent flow and heat transfer in ribbed convergent/divergent rectangular ducts Therm Sci 2015;19(6):2219–31.10.2298/TSCI140107100KSuche in Google Scholar
12 Webb RL, Eckert ERG. Application of rough surface to heat exchanger design Int J Heat Mass Transfer 1972;15(9):1647–58.10.1016/0017-9310(72)90095-6Suche in Google Scholar
13 Kumar S, Saini RP. CFD based performance analysis of a solar air heater duct provided with artificial roughness. Renewable Energy 2009;34:1285–91.10.1016/j.renene.2008.09.015Suche in Google Scholar
© 2018 Walter de Gruyter GmbH, Berlin/Boston
Artikel in diesem Heft
- Frontmatter
- Jet Engines – The New Masters of Advanced Flight Control
- Prediction of Film Cooling Effectiveness on a Gas Turbine Blade Leading Edge Using ANN and CFD
- Sustainability Metrics of a Small Scale Turbojet Engine
- Coupling Network Computing Applications in Air-cooled Turbine Blades Optimization
- Performance Enhancement of One and Two-Shaft Industrial Turboshaft Engines Topped With Wave Rotors
- Semi-Immersive Virtual Turbine Engine Simulation System
- A Novel Modeling Method for Aircraft Engine Using Nonlinear Autoregressive Exogenous (NARX) Models Based on Wavelet Neural Networks
- Defining the Ecological Coefficient of Performance for an Aircraft Propulsion System
- Investigation on the Accuracy of Superposition Predictions of Film Cooling Effectiveness
- Computational Investigations in Rectangular Convergent and Divergent Ribbed Channels
Artikel in diesem Heft
- Frontmatter
- Jet Engines – The New Masters of Advanced Flight Control
- Prediction of Film Cooling Effectiveness on a Gas Turbine Blade Leading Edge Using ANN and CFD
- Sustainability Metrics of a Small Scale Turbojet Engine
- Coupling Network Computing Applications in Air-cooled Turbine Blades Optimization
- Performance Enhancement of One and Two-Shaft Industrial Turboshaft Engines Topped With Wave Rotors
- Semi-Immersive Virtual Turbine Engine Simulation System
- A Novel Modeling Method for Aircraft Engine Using Nonlinear Autoregressive Exogenous (NARX) Models Based on Wavelet Neural Networks
- Defining the Ecological Coefficient of Performance for an Aircraft Propulsion System
- Investigation on the Accuracy of Superposition Predictions of Film Cooling Effectiveness
- Computational Investigations in Rectangular Convergent and Divergent Ribbed Channels