Add to ORKGVisualization and measurements of aerodynamic effects on a delta-wing model and a 2D wing profile were conducted using an optical pressure measurement system, based on the Pressure Sensitive Paint (PSP) technique. The PSP technology provides a good understanding of the flow around the wind tunnel model. The PSP technique can be used to realize absolute pressure measurements on a surface of a model and in addition to evaluate quantitative aerodynamic flow phenomena using scientific grade cameras and image processing technique
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
Visualization and measurements of aerodynamic effects on an 2D-wing-profile model were conducted usi...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile model were conducted usi...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
A two-dimensional and non-intrusive operating optical pressure measurement system PSP (Pressure Sens...
The visualization and measurements of aerodynamic effects on different aircraft models were conducte...
Measurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical press...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing mo...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
Visualization and measurements of aerodynamic effects on an 2D-wing-profile model were conducted usi...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile model were conducted usi...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
A two-dimensional and non-intrusive operating optical pressure measurement system PSP (Pressure Sens...
The visualization and measurements of aerodynamic effects on different aircraft models were conducte...
Measurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical press...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing mo...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...