Developments of Pressure Sensitive Paint (OPMS) for Non-flat Models in Steady Transonic Flow and Unsteady Conditions.
Engler, R. H. (1995) Developments of Pressure Sensitive Paint (OPMS) for Non-flat Models in Steady Transonic Flow and Unsteady Conditions. In: Proceedings 16th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF), Wright-Patterson Air Force Base, Dayton, Ohio, USA, 18-21 July 1995..
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To achieve the diner calibration of pressure sensitive paint of a coated model in the wind tunnel, using the pixel by pixel calibration, a resolution of absolute pressure up to 2mbar in comparison to the conventional PSI technique is possible. However, this is only achieved by using an image processing method for removing image distortions and recording the surface temperature of the model simultaneously. In this case an angular influence of illumination or the resulting emission will be compensated automatically. The results obtained show that in the immediate future the range of application will extend from subsonic into the hypersonic regime. Furthermore, the simultaneous recording of surface temperature will play an increasing role. For exact measurements of unsteady flows a first step was made to acquire periodic flow phenomena. The use of extremely sensitive low-noise video cameras will certainly allow surface pressure measurement of such processes in the future.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1995, pages=9,|
|Title:||Developments of Pressure Sensitive Paint (OPMS) for Non-flat Models in Steady Transonic Flow and Unsteady Conditions.|
|Journal or Publication Title:||Proceedings 16th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF), Wright-Patterson Air Force Base, Dayton, Ohio, USA, 18-21 July 1995.|
|Keywords:||Pressure sensitive paint, measurement technique, wind tunnel, pressure measurements, pressure sensor, optical, luminescence, flow visualization, fluorescence, pressure taps, oil flow pictures.|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||L SI - Versuchs- und Simulationstechniken|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||02 Apr 2006|
|Last Modified:||27 Apr 2009 05:29|
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