Large Eddy Simulations of a piloted lean premix jet flame using finite-rate chemistry

A Large Eddy Simulation (LES) model capable of accurately representing finite-rate chemistry effects in turbulent premixed combustion is presented. The LES computations use finite-rate chemistry and implicit LES combustion modelling to simulate an experimentally well-documented lean-premixed jet flame stabilized by a stoichiometric pilot. The validity of the implicit LES assumption is discussed and criteria are expressed in terms of subgrid scale Damköhler and Karlovitz numbers. Simulation results are compared to experimental data for velocity, temperature and species mass fractions of CH₄, CO and OH. The simulation results highlight the validity and capability of the present approach for the flame and in general the combustion regime examined. A sensitivity analysis to the choice of the finite-rate chemistry mechanism is reported, this analysis indicates that the one and two-step global reaction mechanisms evaluated fail to capture the reaction layer with sufficient accuracy, while a 20-species skeletal mechanism reproduces the experimental observations accurately including the key finite-rate chemistry indicators CO and OH. The LES results are shown to be grid insensitive and that the grid resolution within the bounds examined is far less important compared to the sensitivity of the finite-rate chemistry representation. The results are analyzed in terms of the flame dynamics and it is shown that intense small scale mixing (high Karlovitz number) between the pilot and the jet is an important mechanism for the stabilization of the flame.     

MEPS as a rapid sample preparation method to handle unstable compounds in a complex matrix: determination of AZD3409 in plasma samples utilizing MEPS-LC-MS-MS

The aim of the present investigation is to develop a simple, fast, and sensitive method for the determination of a new candidate drug, AZD3409, in rat, dog, and human plasma samples. AZD3409 is stable in aqueous solutions at low pH (< 4) but not in whole blood or in plasma. In rat plasma at 25 degrees C, more than 90% of the compound is degraded within 40 min. When 20 mg of NaF and 50 microL of protease inhibitor cocktail are added to 1.0 mL of rat blood, AZD3409 is stable for up to about 90 min. Due to the instability of AZD3409, microextraction in packed syringe (MEPS) is used as an online and fast sample-preparation method, followed by liquid chromatography-tandem mass spectrometry (LC-MS-MS) for the quantitation of this compound in plasma samples. In MEPS, the sampling sorbent is 1 mg of polystyrene polymer packed in a 250-microL syringe. When the plasma sample (50-250 microL) is withdrawn through the syringe by an autosampler, the analyte is adsorbed to the solid phase. The analyte is then eluted with an organic solvent such as methanol or the LC mobile phase (20-50 microL) directly into the instrument's injector. MEPS is rapid and easy to use. The lower limit of quantitation for AZD3409 is established to be 0.024 microM. The accuracy of the quality-control samples ranged from 89% to 102%, and the precision (C.V.%) had a value of 11-16% for the plasma samples. The calibration curve in plasma is obtained in the concentration range 0.022-9.0 microM. The coefficients of determination (R2) for plasma samples were > or = 0.998 for all runs. The present method is used for the analysis of rat and dog plasma samples.     

Effects of confinement on premixed turbulent swirling flame using large Eddy simulation

This paper utilises large eddy simulation (LES) to study swirling reacting flows by comparison with experimental observations. The purpose is to provide further insights in engineering designs, as well as to improve modelling. A reduced-scale swirl burner has been developed for the experiments. Comparison of particle image velocimetry (PIV) measurements with LES results using finite rate chemistry shows that LES captures all the salient features of an unconfined flame including velocity and temperature distributions. However, when the flame is confined within a cylindrical combustor, the simulated flame shape is initially not consistent with experimental observation. Investigations show that the discrepancy is caused by the often practised assumption of adiabatic wall temperature. With the use of an assumed wall temperature distribution guided by laboratory observation, results of LES are consistent with experiments. Although the latter LES approach requires more computational resources, the improvement is found to be justified.