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A Comparison of A Single and Multiphase Jets in a Crossflow Using LES
Transcultural novels and translating cultures : François Cheng's Le Dit de Tianyi and L'éternité n'est pas de trop
Noise computation of a turbo-engine jet exhaust based on LES and lighthill's acoustic analogy
Increasing noise regulations at urban airports force jet engine manufactures to develop and build more quiet engines. Over recent years, a significant reduction in fan and mechanical noise has been achieved. However, the jet exhaust is the principal source of noise. The acoustical field that is generated by a turboengine jet exhaust running near the ground level is considered. The full equations o
Study of the vortex breakdown in a conical swirler using LDV, LES and POD
Modeling and understanding the vortex breakdown is a key issue of modern Lean Premixed Combustors. The main difficulty of the problem is the unsteady behavior of this type of flow: Large structures resulting from vortex breakdown and the swirling shear-layers, affect directly the flame stabilization leading to heat-release fluctuations and combustion instabilities. Consequently, one needs to captu
Social movements, social science and politics : von Stein, Le Bon and two persistent problematiques
The growth of social science and sociology during modernity has always been characterized by a will to create predictability for human actions, under the modern conditions of liberty seen as contingent, unpredictable and unstable. To gain systematic knowledge became a way to solve, counteract or radicalize tensions in society, and thus outweighing the risks of contingency. Furthermore, this develo
Numerical studies of flame extinction and re-ignition behaviors in a novel, ultra-lean, non-premixed model GT burner using LES-ESF method
le Critérion (e56), for woodwind quartet (fl, ob, cl, bsn)
La Biennale de Montréal, “Le Grand Balcon/The Grand Balcony”
An extended FGM model with transported PDF for LES of spray combustion
Faustine Perrin
Senior lecturer Contact details Email: faustine [dot] perrin [at] ekh [dot] lu [dot] se Phone: +46 46 222 04 65Organisation Department of Economic History Visiting address: Scheelevägen 15 B, Lund Room number: Alfa 1:2087 Service point: 10 WebpageFaustine Perrins profile in Lund University research portalOther affiliations Senior lecturer Economic demography Senior lecturer Historical labour marke
https://www.lusem.lu.se/faustine-perrin - 2026-04-27
Numerical simulation of a gas-liquid Rushton stirred reactor - LES and LPT
LES and DES of flow and ice accretion on wind turbine blades
LES and DES of flow and ice accretion on wind turbine blades
Implicit les applied to isothermal swirling coaxial jets
Les Houches 2013: Physics at TeV Colliders: Standard Model Working Group Report
Le geste et son double : Plastic Extension of Étude 6 by Heitor Villa-Lobos
Challenging modeling strategies for LES of non-adiabatic turbulent stratified combustion
Five different low-Mach large eddy simulations are compared to the turbulent stratified flame experiments conducted at the Technical University of Darmstadt (TUD). The simulations were contributed by TUD, the Institute for Combustion Technology (ITV) at Aachen, Lund University (LUND), the EM2C laboratory at Ecole Centrale Paris, and the University of Duisburg-Essen (UDE). Combustion is modeled by
LES of the flow and acoustics generated by a wing installed aircraft propeller running in the vicinity of the ground
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
