SUMMARYA preconditioning approach based on the artiÿcial compressibility formulation is extended to solve the governing equations for unsteady turbulent reactive ows with heat release, at low Mach numbers, on an unstructured hybrid grid context. Premixed reactants are considered and a amelet approach for combustion modelling is adopted using a continuous quenched mean reaction rate. An overlapped cellvertex ÿnite volume method is adopted as a discretisation scheme. Artiÿcial dissipation terms for hybrid grids are explicitly added to ensure a stable, discretised set of equations. A second-order, explicit, hybrid Runge-Kutta scheme is applied for the time marching in pseudo-time. A time derivative of the dependent variable is added to recover the time accuracy of the preconditioned set of equations. This derivative is discretised by an implicit, second-order scheme. The resulting scheme is applied to the calculation of an inÿnite planar (one-dimensional) turbulent premixed ame propagating freely in reactants whose turbulence is supposed to be frozen, homogeneous and isotropic. The accuracy of the results obtained with the proposed method proves to be excellent when compared to the data available in the literature.