| Under certain operating conditions, many combustion systems in aerospace propulsion and land-based power generation exhibit large-amplitude pressure oscillations coupled with unsteadiness in the combustion processes. This unsteady multi-scale phenomenon is generally referred to as thermo-acoustic instability. Recently, model-based active control approaches are being pursued to suppress the potentially destructive instability and for this purpose a fundamental understanding of the coupling mechanisms between the dynamics of the flame and acoustics is critical.; In the present investigation, a numerical model is developed to study the interaction of longitudinal acoustic waves with planar flames in the simplified counterflow configuration. The mathematical formulation of quasi one-dimensional, fully unsteady, laminar counterflow flames is derived and the governing equations are integrated numerically based on a MacCormack predictor-corrector scheme, with the inclusion of detailed transport and finite-rate chemistry. In order to accurately represent perfect and partial reflection of acoustic waves at the boundaries, Navier-Stokes characteristic boundary conditions are implemented.; The focus of the investigation is on the linear regime of thermo-acoustic instabilities associated with planar flames. Specifically, coupling mechanisms intrinsic to the dynamics of the flame are addressed, such as flow compressibility effects, which may be responsible for the initial triggering of thermo-acoustic instabilities, and finite-rate chemistry effects. For well-resolved simulations, the occurrence of the self-sustained amplification of pressure fluctuations is analyzed in both non-premixed and premixed methane-air flames for a range of flow strain rates and flame locations, and employing different chemical kinetic models. A detailed analysis of the characteristic time-scales associated with convection, diffusion, chemistry and acoustics is performed together with an analysis of the heat release rate and of the effects of flame location in order to provide a better understanding of the fundamental coupling mechanisms driving the instability, namely chemical kinetic-acoustic coupling and acoustically-induced fluctuations in the mass flux of reactants into the flame. |