This work aims to study the interaction of a shock wave with a cloud of particles to quantify flow unsteadiness and velocity fluctuations using particle-resolved direct numerical simulation (PR-DNS). Three cases are studied, with each case revealing one aspect of the intricate flow phenomena involved in this interaction. The unsteady interaction of a shock wave with a transverse array of particles reveals the origin of unsteadiness under the effect of mutual wave-wave and wave-wake interactions between the particles. In the second case, the interaction of a shock with a particle cloud is studied, with a focus on the interaction of the complex wave system with the vortical structure. A budget analysis of the vorticity equation reveals the so...
The objective of the present research was to extend the Direct Numerical Simulation (DNS) approach t...
Dense compressible multiphase flows exist in variable phase turbines, explosions, and fluidized beds...
International audienceUnder certain circumstances (High Mach number, large shock angle...), the inte...
We investigate the shock-induced flow through random particle arrays using particle-resolved Large E...
International audienceThe effect of shock waves on the dispersion characteristics of a particle clou...
The interaction between a particle and a shock wave leads to unsteady forces that can be an order of...
Dense high speed non-compacted multiphase flows exist in variable phase turbines, explosions, and ej...
An incident shock wave/turbulent boundary layer interaction at Mach 2.1 is investigated using partic...
The spatio-temporal dynamics of an impinging shock/boundary layer interaction atMach 2 and under inc...
Title from first page of PDF file (viewed January 10, 2011)Includes bibliographical references (p. 7...
A fundamental experimental study is carried out to investigate the unsteady flow organization of an ...
International audienceAn LES-based study is presented and focuses on different unsteadiness-source f...
In this paper, the two-dimensional particle-laden flow developments are studied with bronze particle...
The aim of this paper is the direct numerical simulation of the shock wave boundary layer interactio...
A high-speed body, such as a hypersonic aircraft or re-entry vehicle, travelling through weather may...
The objective of the present research was to extend the Direct Numerical Simulation (DNS) approach t...
Dense compressible multiphase flows exist in variable phase turbines, explosions, and fluidized beds...
International audienceUnder certain circumstances (High Mach number, large shock angle...), the inte...
We investigate the shock-induced flow through random particle arrays using particle-resolved Large E...
International audienceThe effect of shock waves on the dispersion characteristics of a particle clou...
The interaction between a particle and a shock wave leads to unsteady forces that can be an order of...
Dense high speed non-compacted multiphase flows exist in variable phase turbines, explosions, and ej...
An incident shock wave/turbulent boundary layer interaction at Mach 2.1 is investigated using partic...
The spatio-temporal dynamics of an impinging shock/boundary layer interaction atMach 2 and under inc...
Title from first page of PDF file (viewed January 10, 2011)Includes bibliographical references (p. 7...
A fundamental experimental study is carried out to investigate the unsteady flow organization of an ...
International audienceAn LES-based study is presented and focuses on different unsteadiness-source f...
In this paper, the two-dimensional particle-laden flow developments are studied with bronze particle...
The aim of this paper is the direct numerical simulation of the shock wave boundary layer interactio...
A high-speed body, such as a hypersonic aircraft or re-entry vehicle, travelling through weather may...
The objective of the present research was to extend the Direct Numerical Simulation (DNS) approach t...
Dense compressible multiphase flows exist in variable phase turbines, explosions, and fluidized beds...
International audienceUnder certain circumstances (High Mach number, large shock angle...), the inte...