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212

Thermo-Fluid Dynamics

High performance simulation with added value

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In 2017 we have made significant progress in the development of modelling concepts and sim-

ulation software for combustion dynamics and combustion noise. Furthermore, consequences of

intrinsic thermoacoustic feedback for the convective scaling of eigenfrequencies were elucidated.

Thomas Emmert was awarded the Dissertation Prize of

the Faculty of Mechanical Engineering for his doctoral

thesis ‘State Space Modeling of Thermoacoustic Systems

with Application to Intrinsic Feedback’.

Wolfgang Polifke and Camilo Silva contributed a course

with the title ‘Systemidentifikation bei Unsicherheiten – Nix

g’naus woas ma ned’ to the Ferienakademie Sarntal.

Research Focus

In recent years, the research efforts of the TFD group have

focused almost exclusively on thermoacoustic combus-

tion instabilities. This type of self-excited instability results

from feedback between fluctuations of heat release rate

and acoustic perturbations of velocity and pressure,

and may occur in combustion applications as diverse as

domestic heaters, gas turbines or rocket engines. Pos-

sible consequences are increased emissions of noise or

pollutants, limited range of operability or severe mechan-

ical damage to a combustor. Thermoacoustic instabilities

have hindered the development of low-emission, reliable

and flexible combustion systems for power generation

and propulsion. Due to their multi-scale and multi-physics

nature, the prediction and control of such instabilities is a

very challenging problem with manifold exciting research

opportunities.

Linearized (Reactive) Flow Solvers

Analysis of thermoacoustic combustion instabilities is

typically based on linearized perturbation equations for

compressible reactive flow, with important effects of

convection by mean flow. A discontinuous Galerkin finite

element method with superior accuracy and stability for

this type of equation has been developed in the TFD

group. Combined with the state-space framework of the

in-house taX software, this method makes possible the

computation of transfer functions and thermoacoustic

Axial velocity of the unstable, intrinsic thermoacoustic eigenmode of a swirl

burner (from Meindl et al., submitted to J. Comp. Phys).

Distribution of heat release rate fluctuations of the intrinsic thermoacoustic

eigenmode of a laminar flame (from Avdonin et al., submitted to Proc.

Combust. Inst., 2018).

eigenmodes with unprecedented speed and flexibility.

Inclusion of a linearized source term for species pro-

duction and heat release allows the explicit inclusion

of flow-flame-acoustic coupling in the computation of

thermoacoustic eigenmodes, which has hitherto not been

possible. Inertial waves as well as entropy waves can also

be described in this framework. First results on the propa-

gation speed of inertial waves, the effect of inertial waves

on flame dynamics, and the source term of entropy waves

have been achieved and published. Such fundamental

investigations of flow-flame-acoustic interactions provide

important guidance for the proper formulation of analysis

and design tools for thermoacoustic stability.

Project

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AG Turbo COOREFLEX, FVV ‘Vorhersage von Flam-

mentransferfunktionen’