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 …

Turbulent swirl flames are known to exhibit intermittent transitions between V-and M-shapes
at certain operating conditions. A diagnostic apparatus based on a commercial highspeed …

This paper presents time-resolved numerical simulations of a well-characterized sooting
swirl flame at elevated pressure. Recently published unsteady Reynolds averaged Navier …

This article presents unsteady Reynolds averaged Navier–Stokes simulations (URANS) of a
well-characterized aero-engine model combustor with finite-rate chemistry (FRC). The …

As almost all combustion processes of practical interest take place in the presence of
turbulence, the development of the increasingly refined turbulence–chemistry interaction …

To enable risk informed decisions in the simulation-based design and development of novel
combustors, uncertainties in the simulation results must be considered. However, due to the …

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 …

This paper presents time-resolved numerical simulations of a well-characterized aero-
engine model combustor. Recently published unsteady Reynolds averaged Navier-Stokes …

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