Add to ORKGMeasurements of aerodynamic effects on a 2D-wing-profile model were conducted using an optical pressure measurement system, based on the pressure-sensitive paint (PSP) technique. The PSP technique has been used here for investigations of periodic and unsteady flows: In a wind tunnel campaign in the DNW-TWG in collaboration with the DLR Institute of Aeroelasticity, a 2D-wing-profile model, which is pitch oscillating at up to 30 Hz, was investigated. For these experiments pressure measurements were carried out in one wind tunnel entry by means of both phase-locked unsteady as well as unsteady PSP techniques
To achieve the diner calibration of pressure-sensitive paint of a coated model in the wind-tunnel, u...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
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 and measurements of aerodynamic effects on a delta-wing model and a 2D wing profile we...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
The visualization and measurements of aerodynamic effects on different aircraft models were conducte...
A two-dimensional and non-intrusive operating optical pressure measurement system PSP (Pressure Sens...
The paper reviews the main problems encountered during investigations of the Oscillating Pressure Fi...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
To achieve the diner calibration of pressure-sensitive paint of a coated model in the wind-tunnel, u...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
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 and measurements of aerodynamic effects on a delta-wing model and a 2D wing profile we...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
The visualization and measurements of aerodynamic effects on different aircraft models were conducte...
A two-dimensional and non-intrusive operating optical pressure measurement system PSP (Pressure Sens...
The paper reviews the main problems encountered during investigations of the Oscillating Pressure Fi...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
Visualization and quantitave measurement of aerodynamic effects on several aircraft models have been...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
To achieve the diner calibration of pressure-sensitive paint of a coated model in the wind-tunnel, u...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...