A two-dimensional time-accurate numerical model to simulate complex reacting flowfields in chemical non-equilibrium is presented. The aim of this studyis to develop a computational tool which permits the analysis and the easy implementation of combustion phenomena for high speed flows. To construct an efficient numerical tool, while maintaining a reasonable accuracy, a semi-implicit numerical method was selected and verified for a hydrogen-air mixture. The numerical approach is based on a time-dependent, finite-volume integration of the governing equations suitably modified for chemical non-equilibrium. The evaluation of the reacting constants based on Gibbs free energy and the Van't Hoff equation allows a very easy implementation of the ch...
Computational fluid dynamics has reached a stage where flow field in practical situation can be pred...
In this paper we describe a numerical algorithm for integrating the multicomponent, reacting, compre...
An adaptive finite volume approach is presented to accurately simulate shock-induced combustion phen...
A two-dimensional time-accurate numerical model to simulate complex reacting flowfields in chemical ...
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
The essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equation...
High-fidelity numerical simulations of combustion processes in next-generation hypersonic propulsion...
The temporal evolution of the combustion process established during projectile transition from the l...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
A new fully implicit, time accurate algorithm suitable for chemically reacting, viscous flows in the...
The shock-induced combustion of methane-air mixtures in hypersonic flows is investigated using a new...
The development and assessment of an efficient parallelization method for the evaluation of reaction...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
Abstract: Numerical simulation of supersonic combustion of hydrogen in air has been done using point...
Computational fluid dynamics has reached a stage where flow field in practical situation can be pred...
In this paper we describe a numerical algorithm for integrating the multicomponent, reacting, compre...
An adaptive finite volume approach is presented to accurately simulate shock-induced combustion phen...
A two-dimensional time-accurate numerical model to simulate complex reacting flowfields in chemical ...
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
The essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equation...
High-fidelity numerical simulations of combustion processes in next-generation hypersonic propulsion...
The temporal evolution of the combustion process established during projectile transition from the l...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
A new fully implicit, time accurate algorithm suitable for chemically reacting, viscous flows in the...
The shock-induced combustion of methane-air mixtures in hypersonic flows is investigated using a new...
The development and assessment of an efficient parallelization method for the evaluation of reaction...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
Abstract: Numerical simulation of supersonic combustion of hydrogen in air has been done using point...
Computational fluid dynamics has reached a stage where flow field in practical situation can be pred...
In this paper we describe a numerical algorithm for integrating the multicomponent, reacting, compre...
An adaptive finite volume approach is presented to accurately simulate shock-induced combustion phen...