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

A Laminar Flamelet Based NOx-Radiation Integrated Modelling of Turbulent Non-Premixed Flame

DOI: 10.1615/ICHMT.2006.TurbulHeatMassTransf.1300
pages 609-612

R.V.V.S. Murthy
Wolfson School of Mechanical and Manufacturing Engineering, Loughborough University, Loughborough, LE11 3TU, Leicestershire, United Kingdom

Weeratunge Malalasekara
Wolfson School of Mechanical, Electrical and Manufacturing Engineering - Loughborough University, Loughborough, LE11 3TU, United Kingdom

Mamdud Hossain
School of Engineering, Robert Gordon University, The Sir Ian Wood Building, Garthdee Road, Aberdeen, AB10 7GJ, United Kingdom


Laminar flamelet model in its adiabatic form has been extended with radiation and NOx sub models to study the impact of radiation heat exchange on NOx predictions. Bluff-body stabilized CH4/H2 flame operating far from blow-off limit has been chosen as the test case. Radiation sub model is based on enthalpy defect concept while NOx model involves solving an additional transport equation for NO with a source term dependent on flamelet calculations. Turbulence closure has been achieved with a modified k-ε model. Detailed chemistry in the form of GRI2.11 has been adopted for the flamelet calculations. Numerical calculations have been carried out in a 2D finite-volume code with staggered grid arrangement. Comparison of predictions from adiabatic and non-adiabatic forms of flamelet model result in similar predictions for mixing field, temperature and major species mass fractions with reasonably good agreement with measurements. The non-adiabatic model however results in minor improvements to NO mass fraction predictions by reducing the extent of overprediction observed with the adiabatic model. In order to achieve this effect, it has been found that variation of scalar dissipation rate should be considered in the non-adiabatic.

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