Доступ предоставлен для: Guest
Главная ICHMT DL Текущий год Архив Исполнительный Комитет ICHMT

Unsteady RANS and Large Eddy Simulation of the flow and heat transfer in a wall bounded pin matrix

DOI: 10.1615/ICHMT.2012.ProcSevIntSympTurbHeatTransfPal.1670
pages 1624-1634

Sofiane Benhamadouche
Fluids Mechanics Energy and Environment Dept., EDF R&D, France

I. Afgan
Modelling & Simulation Centre, School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, M13 9PL Manchester, UK; Institute of Avionics & Aeronautics, Air University, E-9, Islamabad, Pakistan

Frederic Dehoux
EDF R&D, Fluid Mechanics, Energy and Environment Dept., 78401 Chatou, France; Institute Pprime, Dept. Fluid flow, heat transfer and combustion, CNRS−Univ. of Poitiers−ENSMA - SP2MI, teleport 2, 11 bd Marie et Pierre Curie, BP 30179, 86962 Futuroscope Chasseneuil Cedex, France

Remi Manceau
Institute Pprime, Dept. Fluid flow, heat transfer and combustion, CNRS-Univ. of Poitiers-ENSMA, France; Lab. de mathematiques et de leurs applications (LMA) CNRS-Universite de Pau et des pays de I'Adour IPRA, avenue de I'universite 64013 Pau, France; Inria Bordeaux-Sud-Ouest, project-team CAGIRE


Four calculations, two using LES with respectively 18 and 76 million computational cells and two utilizing a URANS approach on a 2 million mesh with sophisticated first and second moment closure approaches; the Ø-model and the EB-RSM combined to the EB-GGDH, have carried out for the flow through a wall bounded pin matrix in a staggered arrangement with a heated bottom wall at a Reynolds number based on the gap velocity and the diameter of the pins equal to 10, 000. Comparisons of the pressure drop, the pressure coefficient distribution, the mean and rms values of the steam-wise velocity component and the Nusselt number distribution along the bottom wall showed clearly that using a first moment closure is not adequate for the present case. Although the wall-resolved LES with 76 million cells shows a superior behavior, the second moment closure exhibits very interesting results.

ICHMT Digital Library

Bow shocks on a jet-like solid body shape. Thermal Sciences 2004, 2004. Pulsed, supersonic fuel jets - their characteristics and potential for improved diesel engine injection. PULSED, SUPERSONIC FUEL JETS - THEIR CHARACTERISTICS AND POTENTIAL FOR IMPROVED DIESEL ENGINE INJECTION
View of engine compartment components (left). Plots of temperature distributions in centreplane, forward of engine (right). CHT-04 - Advances in Computational Heat Transfer III, 2004. Devel... DEVELOPMENT AND CURRENT STATUS OF INDUSTRIAL THERMOFLUIDS CFD ANALYSIS
Pratt & Whitney's F-135 Joint Strike Fighter Engine under test in Florida is a 3600F class jet engine. TURBINE-09, 2009. Turbine airfoil leading edge stagnation aerodynamics and heat transfe... TURBINE AIRFOIL LEADING EDGE STAGNATION AERODYNAMICS AND HEAT TRANSFER - A REVIEW
Refractive index reconstructed field. (a) Second iteration. (b) Fourth iteration. Radiative Transfer - VI, 2010. Theoretical development for refractive index reconstruction from a radiative ... THEORETICAL DEVELOPMENT FOR REFRACTIVE INDEX RECONSTRUCTION FROM A RADIATIVE TRANSFER EQUATION-BASED ALGORITHM
Two inclusion test, four collimated sources. Radiative Transfer - VI, 2010. New developments in frequency domain optical tomography. Part II. Application with a L-BFGS associated to an inexa... NEW DEVELOPMENTS IN FREQUENCY DOMAIN OPTICAL TOMOGRAPHY. PART II. APPLICATION WITH A L-BFGS ASSOCIATED TO AN INEXACT LINE SEARCH