@manual{
	titlea = "Prof.",
	vornamea = "Markus",
	namea = "Klein",
	departmenta = "Fakultät für Luft- und Raumfahrttechnik",
	institutea = "LRT 1 - Institut für Angewandte Mathematik und Wissenschaftliches Rechnen",
	titleb = "",
	vornameb = "",
	nameb = "",
	departmentb = "",
	instituteb = "",
	titlec = "",
	vornamec = "",
	namec = "",
	departmentc = "",
	institutec = "",
	external-funds = "Airbus Defence and Space GmbH",
	company = "",
	project-title = "Efficient Turbulence Modelling for Vortical Flows from Swept Leading Edges",
	project-abstract = "The project aims to develop and optimize an efficient turbulence model suitable for the prediction of the formation and ineraction of leading-edge vortices on multiple-delta configurations, particularly such with control devices on the leading edge to tailor the edge vortices. Based on a classical RANS model like the Spalart-Allmaras model, which has become a general-purpose model in aircraft aerodynamics, the model will be adeapted for an optimal fit to a databse with a wide range of cases. The database will be gained from high-fidelity simulations, i.e. hybrid RANS/LES simulations, which produce the flow field in the most detailed affordable way.",
	proj-beginn = "01.03.2020",
	proj-end = "31.03.2024",
	forschungszentrum = ""
}