G-equation modelling of thermoacoustic oscillations of partially premixed flames. (December 2017)

• Record Type: Journal Article
• Authors: Semlitsch, Bernhard; Orchini, Alessandro; Dowling, Ann P; Juniper, Matthew P
• Is Part Of: International journal of spray and combustion dynamics. Volume 9:Number 4(2017)
• Page Start: 260
• Page End: 276
• Publication Date: 2017-12
• Subjects: Thermoacoustic instability -- non-linear combustion modelling -- flame describing function -- equivalence ratio perturbation; Combustion engineering -- Periodicals; Fluid dynamics -- Periodicals; Combustion -- Periodicals; Spraying -- Periodicals; Combustion; Combustion engineering; Fluid dynamics; Spraying; Periodicals; 541.361
• DOI: 10.1177/1756827717711405
• Languages: English
• ISSNs: 1756-8285

Abstract

Numerical simulations aid combustor design to avoid and reduce thermoacoustic oscillations. Non-linear heat release rate estimation and its modelling are essential for the prediction of saturation amplitudes of limit cycles. The heat release dynamics of flames can be approximated by a flame describing function. To calculate a flame describing function, a wide range of forcing amplitudes and frequencies needs to be considered. For this reason, we present a computationally inexpensive level-set approach, which accounts for equivalence ratio perturbations on flames with arbitrarily complex shapes. The influence of flame parameters and modelling approaches on flame describing functions and time delay coefficient distributions are discussed in detail. The numerically obtained flame describing functions are compared with experimental data and used in an acoustic network model for limit cycle prediction. A reasonable agreement of the heat release gain and limit cycle frequency is achieved even with a simplistic, analytical velocity fluctuation model. However, the phase decay is over-predicted. For sophisticated flame shapes, only the realistic modelling of large-scale flow structures allows the correct phase decay predictions of the heat release rate response.