Robert L. Gordon
University of Melbourne
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Featured researches published by Robert L. Gordon.
Combustion Theory and Modelling | 2007
Robert L. Gordon; Assaad R. Masri; Stephen B. Pope; Graham M. Goldin
This paper presents a numerical study of auto-ignition in simple jets of a hydrogen–nitrogen mixture issuing into a vitiated co-flowing stream. The stabilization region of these flames is complex and, depending on the flow conditions, may undergo a transition from auto-ignition to premixed flame propagation. The objective of this paper is to develop numerical indicators for identifying such behavior, first in well-known simple test cases and then in the lifted turbulent flames. The calculations employ a composition probability density function (PDF) approach coupled to the commercial CFD code, FLUENT. The in-situ-adaptive tabulation (ISAT) method is used to implement detailed chemical kinetics. A simple k–ϵ turbulence model is used for turbulence along with a low Reynolds number model close to the solid walls of the fuel pipe. The first indicator is based on an analysis of the species transport with respect to the budget of convection, diffusion and chemical reaction terms. This is a powerful tool for investigating aspects of turbulent combustion that would otherwise be prohibitive or impossible to examine experimentally. Reaction balanced by convection with minimal axial diffusion is taken as an indicator of auto-ignition while a diffusive–reactive balance, preceded by a convective–diffusive balanced pre-heat zone, is representative of a premixed flame. The second indicator is the relative location of the onset of creation of certain radical species such as HO2 ahead of the flame zone. The buildup of HO2 prior to the creation of H, O and OH is taken as another indicator of autoignition. The paper first confirms the relevance of these indicators with respect to two simple test cases representing clear auto-ignition and premixed flame propagation. Three turbulent lifted flames are then investigated and the presence of auto-ignition is identified. These numerical tools are essential in providing valuable insights into the stabilization behaviour of these flames, and the demarcation between processes of auto-ignition and premixed flame propagation.
Combustion Theory and Modelling | 2009
Robert L. Gordon; Assaad R. Masri; Epaminondas Mastorakos
Data from a recent instantaneous, simultaneous, high-resolution imaging experiment of Rayleigh temperature and laser induced fluorescence (LIF) of OH and CH2O at the base of a turbulent lifted methane flame issuing into a hot vitiated coflow are analysed and contrasted to reference flames to further investigate the stabilization mechanisms involved. The use of the product of the quantified OH and semi-quantified CH2O images as a marker for heat release rate is validated for transient autoigniting laminar flames. This is combined with temperature gradient information to investigate the flame structure. Super-equilibrium OH, the nature of the profiles of heat release rate with respect to OH mole fraction, and comparatively high peak heat release rates at low temperature gradients is found in the kernel structures at the flame base, and found to be indicative of autoignition stabilization.
Combustion Science and Technology | 2014
Jennifer A.M. Sidey; Epaminondas Mastorakos; Robert L. Gordon
This article considers constant-pressure autoignition and freely propagating premixed flames of cold methane/air mixtures mixed with equilibrium hot products at high enough dilution levels to burn within the moderate to intense low oxygen dilution (MILD) combustion regime. The analysis is meant to provide further insight on MILD regime boundaries and to identify the effect of hot products speciation. As the mass fraction of hot products in the reactants mixture increases, autoignition occurs earlier. Species profiles show that the products/reactants mixture approximately equilibrates to a new state over a quick transient well before the main autoignition event, but as dilution becomes very high, this equilibration transient becomes more prominent and eventually merges with the primary ignition event. The dilution level at which these two reactive zones merge corresponds well with that marking the transition into the MILD regime, as defined according to conventional criteria. Similarly, premixed flame simulations at high dilutions show evidence of significant reactions involving intermediate species prior to the flame front. Since the premixed flame governing equations system demands that the species and temperature gradients be zero at the “cold” boundary, flame speed cannot be calculated above a certain dilution level. Up to this point, which again agrees reasonably well with the transition into the MILD regime according to convention, the laminar burning velocity was found to increase with hot product dilution while flame thickness remained largely unchanged. Some comments on the MILD combustion regime boundary definition for gas turbine applications are included.
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 2011
Robert L. Gordon; Christos N. Markides; Epaminondas Mastorakos
This paper details a new experiment designed to investigate the autoignition of an approximately mono-sized fuel droplet stream in a turbulent cross-flow of hot air, a canonical problem of relevance to gas turbine premixers and diesel engines with highly swirling flow. The mean velocity, turbulence characteristics and mean temperature of the air are reported, along with estimated droplet size distribution PDFs. The ignition location downstream from the injection point is measured as a function of the air flow temperature and velocity and droplet generation frequency for ethanol and n-heptane. OH ∗ chemiluminescence movies, recorded at 5 kHz, show that the vapour field autoignites first and droplet-scale combustion occurs later as the droplets pass through the autoignited region. Ethanol, being more volatile that heptane, shows little droplet-scale combustion. Reduction of air temperature by 30 K was found to double the ignition length, a reduction in the droplet size reduced the ignition length, and an increase in air bulk velocity increased the ignition length disproportionally to the average convection time increase, which suggests that evaporation, turbulent mixing, and chemistry all affect the autoignition location. The data can assist the validation of two-phase turbulent combustion models.
Combustion and Flame | 2008
Robert L. Gordon; Assaad R. Masri; Epaminondas Mastorakos
Combustion and Flame | 2007
Robert L. Gordon; Assaad R. Masri; Stephen B. Pope; Graham M. Goldin
Flow Turbulence and Combustion | 2011
Benjamin Böhm; Christof Heeger; Robert L. Gordon; A. Dreizler
Applied Physics B | 2011
V. Weber; J. Brübach; Robert L. Gordon; A. Dreizler
Experiments in Fluids | 2010
C. Heeger; Robert L. Gordon; M.J. Tummers; Thomas Sattelmayer; A. Dreizler
Applied Physics B | 2009
Robert L. Gordon; C. Heeger; A. Dreizler