International audienceEjectors are devices usually made of two convergent-divergent coaxial nozzles which are used to convert pressure energy into kinetic energy. These devices involve very complex phenomena which strongly affect their performance. Flow visualization methods are often used to provide precious information as for the nature of the flow within the ejectors and the comprehension of the physical phenomenaencountered. Unfortunately, the visualization methods used successfully until now in these systems are primarily qualitative techniques. The objective of this paper is to present an attempt at quantitative flow visualization by Particle Image Velocimetry. PIV measurements are conducted in a supersonic air ejector. Several ejecto...
The Particle Image Velocimetry is undoubtedly one of the most important technique in Fluid-dynamics ...
A comprehensive flight test study involving an advanced flow field measurement technique, a particle...
Abstract. An experimental flow study of an axisymmetric body in a supersonic stream with an exhaust ...
International audienceEjectors are devices usually made of two convergent-divergent coaxial nozzles ...
International audienceEjectors are devices usually made of two convergent/divergent coaxial nozzles ...
Particle Image Velocity (PIV) is now a well established, non-intrusive technique for the two dimensi...
Abstract. The extension of particle image velocimetry to supersonic and hyper-sonic wind-tunnel flow...
Particle image velocimetry (PIV) is used to investigate the flow field in a supersonic model combust...
Applying advanced non-intrusive flow visualization techniques to an in-flight environment is a chall...
Particle Image Velocimetry (PIV) has become an important tool in modern flowfield diagnostics, in pa...
The applicability of the Particle Image Velocimetry Method (PIV) as a tool for in-flight flow field ...
A series of experiments have been performed to demonstrate the application of Particle Image Velocim...
Experimental fluid mechanics has for a long time been used to visualize flow phenomenon. An early pi...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
Applying advanced non-intrusive flow visualisation techniques to an in-flight environment is a chall...
The Particle Image Velocimetry is undoubtedly one of the most important technique in Fluid-dynamics ...
A comprehensive flight test study involving an advanced flow field measurement technique, a particle...
Abstract. An experimental flow study of an axisymmetric body in a supersonic stream with an exhaust ...
International audienceEjectors are devices usually made of two convergent-divergent coaxial nozzles ...
International audienceEjectors are devices usually made of two convergent/divergent coaxial nozzles ...
Particle Image Velocity (PIV) is now a well established, non-intrusive technique for the two dimensi...
Abstract. The extension of particle image velocimetry to supersonic and hyper-sonic wind-tunnel flow...
Particle image velocimetry (PIV) is used to investigate the flow field in a supersonic model combust...
Applying advanced non-intrusive flow visualization techniques to an in-flight environment is a chall...
Particle Image Velocimetry (PIV) has become an important tool in modern flowfield diagnostics, in pa...
The applicability of the Particle Image Velocimetry Method (PIV) as a tool for in-flight flow field ...
A series of experiments have been performed to demonstrate the application of Particle Image Velocim...
Experimental fluid mechanics has for a long time been used to visualize flow phenomenon. An early pi...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
Applying advanced non-intrusive flow visualisation techniques to an in-flight environment is a chall...
The Particle Image Velocimetry is undoubtedly one of the most important technique in Fluid-dynamics ...
A comprehensive flight test study involving an advanced flow field measurement technique, a particle...
Abstract. An experimental flow study of an axisymmetric body in a supersonic stream with an exhaust ...