Time resolved digital high speed image recording of flow properties using schlieren and shadowgraph methods have become a standard tool in today’s investigations of hypersonic flows. Postprocessing is often necessary to enhance image quality, followed by quantitative image analysis to measure important flow features. Therefore, a software has been developed allowing flexible design of evaluation workflows and a high degree of automatization. Evaluation of shock stand-off distance and shock angle in experimental visualization series at HEG can be carried out. Even force prediction based on analysis of model displacement has been realized. The tool and design considerations based on typical problems of hypersonic flow visualization are discus...
A low-cost, robust, versatile digital shadowgraph visualization system is presented that provides a ...
The Background Oriented Schlieren (BOS) technique is a method that has been developed recently for e...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
AbstractA digital image processing algorithm was developed to identify flow patterns in high speed i...
Optical imaging techniques have played a major role in understanding the flow dynamics of varieties ...
Optical imaging techniques have played a major role in understanding the flow dynamics of varieties ...
Schlieren and shadowgraph photography has been widely used to offer insight into the flow field in a...
Experiments to demonstrate the use of the background-oriented schlieren (BOS) technique in hypersoni...
Schlieren and shadowgraph photography has been widely used to offer insight into the flow field in a...
Visualisation of supersonic compressible flows using the Background Oriented Schlieren (BOS) techniq...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
A low-cost, robust, versatile digital shadowgraph visualization system is presented that provides a ...
The Background Oriented Schlieren (BOS) technique is a method that has been developed recently for e...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...
AbstractA digital image processing algorithm was developed to identify flow patterns in high speed i...
Optical imaging techniques have played a major role in understanding the flow dynamics of varieties ...
Optical imaging techniques have played a major role in understanding the flow dynamics of varieties ...
Schlieren and shadowgraph photography has been widely used to offer insight into the flow field in a...
Experiments to demonstrate the use of the background-oriented schlieren (BOS) technique in hypersoni...
Schlieren and shadowgraph photography has been widely used to offer insight into the flow field in a...
Visualisation of supersonic compressible flows using the Background Oriented Schlieren (BOS) techniq...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
This paper presents a technique to automatically detect flow structures recorded in schlieren images...
A low-cost, robust, versatile digital shadowgraph visualization system is presented that provides a ...
The Background Oriented Schlieren (BOS) technique is a method that has been developed recently for e...
Measurements of aerodynamic forces and moments in ground-based hypersonic shock tunnels are complica...