A detailed experimental investigation of the influence of small gaps on a pseudo-shock system has been performed for different gap sizes and pressure ratios p02/p01. In addition to schlieren images that only provide integral information of the total light deflection through the test section, 3-D numerical data was additionally used to investigate 3-D phenomena of the shock system. The combination of experimental and numerical techniques considerably increased the understanding of the underlying mechanisms that cause the change in structure and position of the pseudo-shock system when increasing the gap size
Moderately under-expanded jets issuing from a circular baseline and two bevelled circular nozzles im...
Vortex loops are fundamental building blocks of supersonic free jets. Isolating them allows for an e...
National Ignition Facility targets, especially those made with material such as beryllium through wh...
A pseudo-shock system in a rectangular nozzle with parallel side walls is investigated at different ...
The scope of this work is to investigate the structure and stochastic asymmetry of pseudo-shock syst...
In the frame of the project "Gasdynamically initiated nanoparticle production", detailed numerical a...
In order to perform Schlieren visualizations of transonic nozzle flows, quartz glass windows are mou...
AbstractWhen the pressure ratio increases from the perfectly expanded condition to the third limited...
The flow in a Supersonic Injection Feeder involves relatively thick boundary layers in a narrow chan...
Supersonic air jets from the D'Laval nozzle of designed Mach number 2.0 were experimentally investig...
When the pressure ratio increases from the perfectly expanded condition to the third limited conditi...
The performance of liquid rocket engines is presently limited by the side loads that take place duri...
It is well known that when a shock-boundary layer interaction is comparatively strong, the shock in ...
The thermo-structural response of solid rocket motor nozzles is widely investigated in the design of...
Underexpanded jets from oval sonic nozzles were experimentally studied for various pressure ratios u...
Moderately under-expanded jets issuing from a circular baseline and two bevelled circular nozzles im...
Vortex loops are fundamental building blocks of supersonic free jets. Isolating them allows for an e...
National Ignition Facility targets, especially those made with material such as beryllium through wh...
A pseudo-shock system in a rectangular nozzle with parallel side walls is investigated at different ...
The scope of this work is to investigate the structure and stochastic asymmetry of pseudo-shock syst...
In the frame of the project "Gasdynamically initiated nanoparticle production", detailed numerical a...
In order to perform Schlieren visualizations of transonic nozzle flows, quartz glass windows are mou...
AbstractWhen the pressure ratio increases from the perfectly expanded condition to the third limited...
The flow in a Supersonic Injection Feeder involves relatively thick boundary layers in a narrow chan...
Supersonic air jets from the D'Laval nozzle of designed Mach number 2.0 were experimentally investig...
When the pressure ratio increases from the perfectly expanded condition to the third limited conditi...
The performance of liquid rocket engines is presently limited by the side loads that take place duri...
It is well known that when a shock-boundary layer interaction is comparatively strong, the shock in ...
The thermo-structural response of solid rocket motor nozzles is widely investigated in the design of...
Underexpanded jets from oval sonic nozzles were experimentally studied for various pressure ratios u...
Moderately under-expanded jets issuing from a circular baseline and two bevelled circular nozzles im...
Vortex loops are fundamental building blocks of supersonic free jets. Isolating them allows for an e...
National Ignition Facility targets, especially those made with material such as beryllium through wh...