Pressure Sensitive Paint (PSP)

Measured values

  • Pressure

Principle

The PSP technique is an optical measurement method, which provides a pressure measurement on surfaces without introducing flow-disturbing probes and without affecting the surface of the model. To obtain the surface pressure by this method, the model is coated with a special paint, which is illuminated for example by UV light. The intensity of the resulting fluorescence light depends on the local oxygen concentration and allows for the determination of the two-dimensional pressure distribution.

While conventional pressure measurement methods are only capable to measure the pressure distribution on discrete points on the surface by installing pressure sensors such as taps and transducers, the two-dimensional PSP method provides a measurement of the entire surface. In addition, due to a better spatial resolution, disturbances in the flow are observable. Furthermore, costs for taps and transducers and for their installation can be saved. Finally, a major drawback of conventional pressure measurement technique is avoided by using PSP: The location of pressure taps must be determined prior to model manufacturing, at a time when the flow pattern is not known exactly. Also there are restrictions to drill holes in thin parts of wind tunnel models in order to install taps and transducers. These restrictions do not apply for a PSP coating applied to the surface of the model with a spray gun.

Generally, the PSP technique is based on an oxygen quenching process in which photo-chemical molecules excited by light are deactivated by collisions with oxygen molecules in spite of irradiation of fluorescence light. This leads to different degrees of luminosity on the surface of the model depending on the local pressure. A final pressure map is obtained from images of CCD cameras using complex image processing techniques. With the software ToPas developed at DLR, such pressure maps are made available during the test.

The sensitivity of the employed optical pressure sensor, which is DLR’s own “binary paint”, has been optimized in the pressure range of 0.1 – 1.5 bar. This is the typical pressure range, observable on models within the transonic flow range. Nevertheless the mobile DLR-PSP system has been successfully used for applications in low speed and hypersonic wind tunnels. Under static conditions a resolution of around ± 1.5 mbar with a response time of 0.5 s can be achieved. For unsteady investigations, ”faster” paints are under development with shorter response times, but with a lower accuracy in absolute pressure.

Application

At the DLR Institute of Aerodynamics and Flow Technology the application of pressure sensitive paint (PSP) is used as a tool to determine the pressure distribution on aircraft surfaces during aircraft design processes. Instantaneous two-dimensional pressure distributions on the surface of a model in test facilities like wind tunnels or turbo machines are considered a major advancement in the field of non-intrusive measurement techniques within aerodynamics.

Applications

  • Transonic flows
  • Low speed flows
  • Hypersonic and short duration flows
  • Unsteady flows

Literature / References

  • [1] Engler R H, Hartmann K, Schulze B, 1991 A new optical pressure measurement sys-tem (OPMS) , ICIASF' 91 Record, Rockville, Maryland, USA, 163-170
  • [2] Engler R H, Hartmann K, Troyanovski I, Vollan A, 1992 Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed wind tunnel of DLR in Göttingen , DLR-FB 92-24, 1-66
  • [3] Engler R H, 1995 Further developments of pressure sensitive paint (OPMS) for non flat models in steady transonic flow and unsteady conditions ICIASF'95 Record, Dayton. Ohio. USA, 163-170
  • [4] Engler R H, Klein Chr, 1997 Optical Pressure Measurement (PSP), Optical Flow Measurement Advanced School, Udine, Italy
  • [5] Engler R H, Klein Chr, 1997 First Results Using the New DLR PSP system - intensity and lifetime measurements; Conference "Wind Tunnels and Wind Tunnel Test Tech-niques", Cambridge UK, ISBN 185768 048 0
  • [6]Klein Chr., 1997, Einsatz einer druckempfindlichen Beschichtung (PSP) zur Bestimmung des momentanen Druckfeldes von Modellen im Windkanal. Dissertation University Göttingen, Germany, DLR-Forschungsbericht 97-55, ISSN 1434-8454, 1997.

Institute / Organization

Institute of Aerodynamics and Flow Technology

Contact

Dr.rer.nat. Christian Klein
Institute of Aerodynamics and Flow Technology

Dr. Frank Holtmann
Technology Marketing

Similar Measures

Subsequent references to data sheets are given which describe with high probability similar measured values. The selection is made on the basis of semantic affinity:

Pressure :: more