Direct numerical simulations of turbulent reacting flows were performed to study the interaction between chemical heat release and turbulent fluid motion. A portion of the energy released by exothermic reactions is placed in the compressible mode of turbulent kinetic energy, with very little energy disposed to the incompressible mode. This process results in a positive feedback mechanism, whereby temperature fluctuations are amplified by the chemical reactions. In the case of endothermic reactions, the feedback is negative, resulting in decreased turbulent motion. The results of the simulations were used to develop a model for temperature fluctuations under conditions typical of a hypersonic boundary layer. This model has been validated and...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
We study a class of chemically reacting, spatially evolving, supersonic mixing layers via large eddy...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
Les effets de haute température survenant lors des vols hypersoniques ont un impact sur les performa...
The influence of high-enthalpy effects on hypersonic turbulent boundary layers is investigated by me...
A hypersonic turbulent boundary layer over a flat plate is numerically investigated. The large Mach ...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
The direct numerical simulation (DNS) data of a turbulent, reacting boundary layer is used to study ...
A hypersonic, spatially evolving turbulent boundary layer at Mach 12.48 with a cooled wall is analys...
The research on shock wave/turbulent boundary-layer interactions is mainly limited to calorically pe...
In this paper, we investigate the eect of turbulence uctuations on surface heating rate by conducti...
Understanding non-equilibrium effects of hypersonic turbulent boundary layers is essential in order ...
We study a class of chemically reacting, spatially evolving, supersonic mixing layers via large eddy...
The research on shock wave/turbulent boundary-layer interactions is mainly limited to calorically pe...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
We study a class of chemically reacting, spatially evolving, supersonic mixing layers via large eddy...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
Les effets de haute température survenant lors des vols hypersoniques ont un impact sur les performa...
The influence of high-enthalpy effects on hypersonic turbulent boundary layers is investigated by me...
A hypersonic turbulent boundary layer over a flat plate is numerically investigated. The large Mach ...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
International audienceThe influence of high-enthalpy effects on hypersonic turbulent boundary layers...
The direct numerical simulation (DNS) data of a turbulent, reacting boundary layer is used to study ...
A hypersonic, spatially evolving turbulent boundary layer at Mach 12.48 with a cooled wall is analys...
The research on shock wave/turbulent boundary-layer interactions is mainly limited to calorically pe...
In this paper, we investigate the eect of turbulence uctuations on surface heating rate by conducti...
Understanding non-equilibrium effects of hypersonic turbulent boundary layers is essential in order ...
We study a class of chemically reacting, spatially evolving, supersonic mixing layers via large eddy...
The research on shock wave/turbulent boundary-layer interactions is mainly limited to calorically pe...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
We study a class of chemically reacting, spatially evolving, supersonic mixing layers via large eddy...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...