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The hybrid RANS/LES of partially premixed supersonic combustion using G/Z flamelet model
L.E. v. Greece: Human Trafficking and the Scope of States’ Positive Obligations under the ECHR
A standard format for Les Houches Event Files
LES of the flow and acoustics generated by an aircraft fan running in the vicinity of the ground
LES of the flow and particle ingestion into an air intake of a jet engine running on the ground
The flow field generated by the flow into a jet engine air-intake, with near ground effects, is considered. The axial inflow in the neighborhood of the ground generates a system of unsteady vortices. Some of these vortices extend from the air-intake towards the ground. Some of these vortices are strong enough to dislocate and even lift small objects from the ground up to the air-intake. The dynami
Le , guo and zhe in Mandarin Chinese: a relevance-theoretic account
LES of Jets and Sprays Injected into Crossflow
The objective of this thesis is to numerically simulate a fluid jet injected into a crossflow of the same or another fluid, respectively. Such flows are encountered in many engineering applications in which cooling or mixing plays an important role, e.g. gas turbine combustors. The jet in crossflow (JICF) is used both for cooling and for injecting liquid fuel into the air stream prior to combustio
Numerical simulation of a gas-liquid Rushton stirred reactor - LES and LPT
LES of the flow and acoustics generated by a wing installed aircraft propeller running in the vicinity of the ground
Les Houches 2017: Physics at TeV Colliders Standard Model Working Group Report
LES investigation of heat transfer in a tube with irregular roughness at moderate Prandtl numbers
Wall-bounded turbulent flows are central to a wide range of engineering applications, where surface roughness can significantly influence both frictional drag and convective heat transfer. While the momentum effects of roughness have been significantly advanced in the literature, the thermal counter parts remain insufficiently understood. This study addresses the critical gap in understanding roug
Resistance and Agency in Peter S. Beagle’s The Last Unicorn and Ursula K. Le Guin’s “The Ones Who Walk Away from Omelas”
LES of Biomass Syngas Combustion in a Swirl Stabilised Burner : Model Validation and Predictions
Characteristics of MILD combustion of CH4-CO2 jets in a piloted burner – Laser-diagnostic and LES studies
Fundamental characteristics of the reaction-zone structure for CH4-CO2 jets, mimicking a fuel of high CO2 contents such as biogas, burning in a heated coflow on a piloted jet burner have been investigated. Jet flames under diffusion and MILD combustion conditions were studied using planar laser-induced fluorescence (PLIF) of O-atom radicals and CO for different CO2 contents of the fuel jet. Numeri
LES modeling of the DLR generic single-cup spray combustor : comparison of exploratory category C jet fuels
LES study of diesel flame/wall interaction and mixing mechanisms at different wall distances
In this paper, the flame-wall interaction of reacting diesel spray under engine like conditions is investigated using large eddy simulations. The aim of this study is to understand the influence of the distance between the wall and the spray nozzle on the air entrainment rate, which is a key variable in formation/oxidation process of soot. Three experimental cases are investigated, a free jet case
A comparison of a single- and multiphase jets in a crossflow using LES
Large eddy simulations are performed for a single- and multiphase jets in crossflow (JICF). The multiphase JICF are compared to the single-phase case for the same momentum and mass flow ratios but with droplets of different sizes. Multiphase JICF have stronger counter-rotating vortex pairs (CVPs) than a corresponding single-phase JICF. Moreover, their trajectories are higher and their induced wake
The lithostratigraphy of the Les Echets basin, France: tentative correlation between cores
A numerical comparison of the thermoacoustics for different equivalence ratios for n-dodecane using LES
Klimatförändringarna påverkar vår värld och det behövs ett mer hållbart samhälle. Flygindustrin är i behov av förändring, men flygmotorer är mycket komplexa och tar tid att utveckla. Termoakustiska instabiliteter har kraften att förstöra en motor, men också att minska miljöpåverkan. Samtidigt möjliggör ökad beräkningskraft i moderna datorkluster att detaljerade simuleringar kan utföras för att stuClimate change is affecting our world and a more sustainable society is needed. The aviation industry is in need of change but aero-engines are very complex and take time to develop. Thermoacoustic instabilities have the power to destroy an engine, but also to reduce the environmental impact. At the same time, increasing computational power allows detailed simulations to be executed in order to st
