A combustion model based on a flamelet/progress variable approach for high-speed flows is
introduced. In the proposed formulation, the temperature is computed from the transported …

The flamelet approach for non-premixed combustion is based on the description of the
turbulent flame as a collection of laminar flame elements embedded in a turbulent flow and …

The flamelet method has been used extensively as an affordable turbulence-combustion
interaction model that obviates the need to solve the evolution equations for the species …

Two flamelet-type models are developed for supersonic combustion flows. First, the
representative interactive flamelet (RIF) model is introduced to fully incorporate the local …

The renewed interest in high-speed flight has recently demonstrated the need for the
development of hypersonic air-breathing propulsion systems, ie, in which the ambient air is …

In this study, large eddy simulations (LES) of supersonic combustion using a compressible
flamelet/progress variable (CFPV) approach are performed for the HIFiRE scramjet at Mach …

A numerical method is presented for the simulation of turbulent diffusion flames in complex
compressible flow fields. The method uses a two equation k-ϵ turbulence model combined …

Three-dimensional calculations of turbulent combustion which include ignition, laminar and
turbulent flame propagation and quenching at the wall are performed by the coherent …

To account for compressibility effects on chemistry in supersonic combustion, a new
linearized correction applied to a flamelet-based model incorporating a progress variable is …

This paper has the objective of addressing a few basic issues pertaining to the use of the
laminar flamelet method to model turbulence-combustion interactions in supersonic …