International audienceThe flow in a planar overexpanded nozzle with a slope discontinuity is studied numerically by means of two- (2D) and three-dimensional (3D) Reynolds-averaged Navier-Stokes simulations and is compared to experimental results. The nozzle pressure ratios (NPR) vary from 1.6 to 10. A good agreement is found between experimental and numerical results and two configurations are observed: under a certain critical NPR, the flow is shown to be asymmetrical with respect to the nozzle axis, while it is perfectly symmetrical for higher NPRs. The value of the critical NPR is found to be very dependent on the turbulence model. Finally, an hysteresis phenomenon is evidenced since the NPR at which the change of flow configuration occu...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...
Experiments, simulations, and numerical bifurcation analysis are used to study the incompressible fl...
Three dimensional solutions of a single expansion ramp nozzle are computed with the existing PARC co...
The flow in an Over-Expanded Nozzle is subjected to shock waves leading to the unsteady separation o...
The compressible jet plume from a planar overexpanded nozzle is investigated by solving the Reynolds...
This paper presents numerical and experimental findings regarding flow separation phenomenon in a hi...
The current paper discusses the exhaust flow features and the various unsteady flow separation chara...
Turbulent flow separation in over-expanded rocket nozzles is investigated numerically in a sub-scale...
Flow separation in rocket nozzles is undesirable because of its unsteady and nonsymmetric nature, wh...
Separation of supersonic flow in a planar convergent-divergent nozzle with moderate expansion ratio ...
The performance of liquid rocket engines is presently limited by the side loads that take place duri...
Numerical simulations of overexpanded rocket nozzle flows show three kinds of flow separation struct...
Flow through a two-dimensional supersonic ConvergentDivergent nozzle with a rectangular cross sectio...
The flow in the divergent part of a highly over-expanded nozzle suffers strong instability due to fo...
A two dimensional convergent-divergent nozzle with a rectangular cross section is modelled under amb...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...
Experiments, simulations, and numerical bifurcation analysis are used to study the incompressible fl...
Three dimensional solutions of a single expansion ramp nozzle are computed with the existing PARC co...
The flow in an Over-Expanded Nozzle is subjected to shock waves leading to the unsteady separation o...
The compressible jet plume from a planar overexpanded nozzle is investigated by solving the Reynolds...
This paper presents numerical and experimental findings regarding flow separation phenomenon in a hi...
The current paper discusses the exhaust flow features and the various unsteady flow separation chara...
Turbulent flow separation in over-expanded rocket nozzles is investigated numerically in a sub-scale...
Flow separation in rocket nozzles is undesirable because of its unsteady and nonsymmetric nature, wh...
Separation of supersonic flow in a planar convergent-divergent nozzle with moderate expansion ratio ...
The performance of liquid rocket engines is presently limited by the side loads that take place duri...
Numerical simulations of overexpanded rocket nozzle flows show three kinds of flow separation struct...
Flow through a two-dimensional supersonic ConvergentDivergent nozzle with a rectangular cross sectio...
The flow in the divergent part of a highly over-expanded nozzle suffers strong instability due to fo...
A two dimensional convergent-divergent nozzle with a rectangular cross section is modelled under amb...
As a part of an aerodynamics Ecole Polytechnique project, separation modes which occur in supersonic...
Experiments, simulations, and numerical bifurcation analysis are used to study the incompressible fl...
Three dimensional solutions of a single expansion ramp nozzle are computed with the existing PARC co...