The essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equations is extended to solve a system of coupled conservation equations governing two-dimensional, time-dependent, compressible chemically reacing flow with full chemistry. The thermodynamic properties of the mixture are modeled accurately, and stiff kinetic terms are separated from the fluid motion by a fractional step algorithm. The methodology is used to study the concept of shock-induced mixing and combustion, a process by which the interaction of a shock wave with a jet of low-density hydrogen fuel enhances mixing through streamwise vorticity generation. Test cases with and without chemical reaction are explored here. Our results indicat...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
Previous work by these authors analyzed in depth vorticity generation and transport in supersonic fl...
The hypervelocity two-dimensional reacting supersonic mixing layer experiments of Erdos et al. with ...
The essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equation...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
summary:During the last years the interest in the numerical simulation of reacting flows has grown c...
In this paper we use numerical simulation to investigate shock-induced ignition and combustion of a...
A two-dimensional time-accurate numerical model to simulate complex reacting flowfields in chemical ...
This document is divided into two parts. Part A, on turbulent transport of chemical species in compr...
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
Significant contributions were made in a four-year interdisciplinary experimental, numerical and the...
This contribution summarizes the state of the art concerning the simulation with computational fluid...
In air breathing propulsion systems for flight at Mach numbers 7 to 20, it is generally accepted tha...
This computational study is a direct simulation calculation of high speed reacting and non-reacting ...
Combustion is an important phenomenon in many engineering applications; com-bustion of hydrocarbons ...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
Previous work by these authors analyzed in depth vorticity generation and transport in supersonic fl...
The hypervelocity two-dimensional reacting supersonic mixing layer experiments of Erdos et al. with ...
The essentially nonoscillatory (ENO) shock-capturing scheme for the solution of hyperbolic equation...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
summary:During the last years the interest in the numerical simulation of reacting flows has grown c...
In this paper we use numerical simulation to investigate shock-induced ignition and combustion of a...
A two-dimensional time-accurate numerical model to simulate complex reacting flowfields in chemical ...
This document is divided into two parts. Part A, on turbulent transport of chemical species in compr...
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
Significant contributions were made in a four-year interdisciplinary experimental, numerical and the...
This contribution summarizes the state of the art concerning the simulation with computational fluid...
In air breathing propulsion systems for flight at Mach numbers 7 to 20, it is generally accepted tha...
This computational study is a direct simulation calculation of high speed reacting and non-reacting ...
Combustion is an important phenomenon in many engineering applications; com-bustion of hydrocarbons ...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
Previous work by these authors analyzed in depth vorticity generation and transport in supersonic fl...
The hypervelocity two-dimensional reacting supersonic mixing layer experiments of Erdos et al. with ...