Application of the PSP technique in low speed wind tunnels

Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Volumn 92, Issue , 2006, Pages

  Henne, U ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84872795052     PISSN: 16122909     EISSN: None     Source Type: Book Series    
DOI: 10.1007/978-3-540-33287-9_6     Document Type: Article

References (7)

1. 2-druckabhängigen Lumineszenz für die Anwendung als Pressure Sensitive Paint. Dissertation University Göttingen, Germany, DLR-FB 2004-18, 2004.
2. R.H. Engler, et al. 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, 1992.
3. R.H. Engler and Chr. Klein. First Results Using the New DLR PSP System -Intensity and Lifetime Measurements, Conference "Wind Tunnels and Wind Tunnel Test Techniques", Cambridge UK, ISBN 185768 048 0, 1997.
4. th ICIASF, Göttingen, Germany, ISBN 0-7803-8149-1, 2003.
5. M. Huhnd, Discretion of Air Motors DA 40/15000 for use on Wind Tunnel Model FLA 5+10, Laboratory Instrumentation Note, Airbus Deutschland GmbH, M72D04024103, 2004.
6. J. Meyer, et al. System Layout and Instrumentation of a Laminar Flow System for the DLR Do228 Test Vehicle, RaeS Aerospace Aerodynamics Research Conference, London, 2003.
7. A. Quast, Detection of Transition by Infrared Image Technique, IEEE publication CH2449-7/87, ICIASF 1987, 1987.