The thermoacoustic oscillation of a turbulent, swirl-stabilized, partially premixed flame in the
PRECCINSTA gas turbine model combustor is analyzed by means of a Scale Adaptive …

The computation of combustion instabilities requires efficient numerical solvers. For low
Mach number compressible flows splitting schemes provide an adequate family of solution …

A method for selective, frequency-resolved analysis of spatially distributed, time-coherent
data is introduced. It relies on filtering of Fourier-processed signals with periodic structures …

Scale Adaptive Simulations (SAS) of the swirl-stabilized flame of the PRECCINSTA burner
are presented. Within the computations a large share of velocity fluctuations as well as …

The computation of low Mach number self-excited thermoacoustic instabilities using large
eddy simulations requires an efficient compressible, multi-species, reacting flow solver …

The computation of self-excited thermoacoustic instabilities remains a challenging task.
Reasons are manifold as the problem renders itself as a complex interplay of mixing …

VT-Forschungsbericht 2016-01 Page 1 Numerische Simulation von thermoakustischen
Instabilitäten in Gasturbinenbrennkammern mithilfe von Impedanzrandbedingungen VT-Forschungsbericht …

Combustion noise in the laboratory scale PRECCINSTA (prediction and control of
combustion instabilities in industrial gas turbines) burner is simulated with a new, robust …

Addressing the pressing need for reduced carbon emissions, Turbulent Jet Ignition (TJI)
emerges as a promising technology for ultra-lean combustion, offering enhanced thermal …

5.2. 8 Identifikation der Beiträge zum Strahlflammen-Lärmspektrum mithilfe der
semianalytischen Analyse aus Abbildung 5.2. 7..................... 106 5.3. 1 Beispielhafte …