The capability of the Pressure-Sensitive Paint (PSP) method for application in unsteady flows in cryogenic wind tunnels was investigated by carrying out experiments in the Cryogenic Ludwieg-Tube Göttingen (KRG). The 2D airfoil model (LV2F) was coated with PtTFPP/PTMSP paint and tested in a nitrogen atmosphere between 120 – 283 K. PSP and pressure tap data were acquired at different Mach and Reynolds number. The oxygen concentration of the flow was set to approx. 1000 ppm by preconditioning supplying dry air. As a result, the intensity-based PSP method successfully measured the pressure distribution on the airfoil model under cryogenic conditions and clearly the expected shock oscillation could be detected and resolved by means of PSP. There...
The pressure sensitive paint (PSP) intensity and lifetime system is an optical measurement technique...
A modification to the Pressure Sensitive Paint (PSP) method was used to visualize streamlines on a B...
Measurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical press...
The capability of the Pressure-Sensitive Paint (PSP) method for application in unsteady flow in cryo...
The capability of the Pressure-Sensitive Paint (PSP) method for application in unsteady flow in cryo...
The capability of a lifetime-based Pressure-Sensitive Paint (PSP) method for application in cryogeni...
Temperature-Sensitive Paint (TSP) and Pressure-Sensitive Paint (PSP) technique have been applied in ...
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...
Pressure-Sensitive Paint (PSP) applied to the wing surface of a full-span airplane model was tested ...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
An investigation by means of the Pressure-Sensitive Paint {PSP) technique for the use in the Europea...
For investigations of pressure distri¬butions on wind tunnel model surfaces with high spatial resolu...
Visualization and measurements of aerodynamic effects on an 2D-wing-profile model were conducted usi...
The pressure sensitive paint (PSP) intensity and lifetime system is an optical measurement technique...
A modification to the Pressure Sensitive Paint (PSP) method was used to visualize streamlines on a B...
Measurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical press...
The capability of the Pressure-Sensitive Paint (PSP) method for application in unsteady flow in cryo...
The capability of the Pressure-Sensitive Paint (PSP) method for application in unsteady flow in cryo...
The capability of a lifetime-based Pressure-Sensitive Paint (PSP) method for application in cryogeni...
Temperature-Sensitive Paint (TSP) and Pressure-Sensitive Paint (PSP) technique have been applied in ...
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...
Pressure-Sensitive Paint (PSP) applied to the wing surface of a full-span airplane model was tested ...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
An investigation by means of the Pressure-Sensitive Paint {PSP) technique for the use in the Europea...
For investigations of pressure distri¬butions on wind tunnel model surfaces with high spatial resolu...
Visualization and measurements of aerodynamic effects on an 2D-wing-profile model were conducted usi...
The pressure sensitive paint (PSP) intensity and lifetime system is an optical measurement technique...
A modification to the Pressure Sensitive Paint (PSP) method was used to visualize streamlines on a B...
Measurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical press...