Particle image velocimetry as validation tool in aeronautics

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Schroder A ^a   Pallek, D ^a   Geisler, R ^a   Lauke, T ^a   Herr, M ^a   Geyr, H V ^a   Dierksheide, U ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b LAVISION GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FLUID MECHANICS; OPTICAL DATA PROCESSING; VELOCITY; VELOCITY MEASUREMENT; WIND TUNNELS;

AERONAUTICAL RESEARCH; FLUCTUATION VELOCITIES; HIGH SPATIAL RESOLUTION; MEASUREMENT TECHNIQUES; OPTICAL MEASUREMENT TECHNIQUES; PARTICLE IMAGE VELOCIMETRIES; SOUND PRESSURE WAVES; VELOCITY VECTOR FIELD;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78549289863     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-1518     Document Type: Conference Paper

References (20)

1. Klein, Christian (2008): Recent Developments of PSP and TSP at DLR for Application to Transonic Flows in Industrial Wind Tunnels., 2008 AIAA Meeting Papers on Disc (DVD-ROM), Vol. 13 (No. 1), S. 33 Folien 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV (USA), 2008-01-07 - 2008-01-10, ISBN 978-1-56347-937-3.
2. Konrath, R.; Klein, C.; Schröder, A.; Kompenhans, J. (2008): Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing. Rockwell, D.; Tropea, C. [Hrsg.]: Experiments in Fluids, Experimental Methods and their Applications to Fluid Flow, Vol. 44 (3), Springer Verlag Berlin/Heidelberg, S. 357 - 366, ISSN 0723-4864 (print), 1432-1114 (online), DOI: 10.1007/s00348-007-0445-5.
3. Kirmse, Tania (2007): Model deformation measurements in DNW-NWB within the DLR project ForMEx., Conference Proceedings, CD-ROM (S12-1), S. 1 - 14 ODAS 2007 - 8th ONERA-DLR Aerospace Symposium, Göttingen, Germany, 2007-10-17 - 2007-10-19.
4. Egami, Yasuhiro; Fey, Uwe; Quest, Jürgen (2007): Development of New Two-Component TSP for Cryogenic Testing. In: American Institue of Aeronautics and Astronautics [Hrsg.]:, Conference Proceedings online (AIAA-2007-1062), S. 1 - 11 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 2007-01-08 - 2007-01-11.
5. Koop, Lars; Ehrenfried, Klaus (2008): Microphone-array processing for wind-tunnel measurements with strong background noise., AIAA Conference Proceedings CD-ROM, Session 16-AA-16 (AIAA 2008-2907), S. 1 - 20 14th AIAA/CEAS Aeroacoustics Conference, Vancouver (Canada), 2008-05-05 - 2008-05-07.
6. Roosenboom, Eric; Schröder, Andreas; Kompenhans, Jürgen (2008): BOS measurements in propeller slipstream., CDROM Conference Proceedings (Paper 274) 13th International Symposium on Flow Visualization, Nice (France), 2008- 07-01 - 2008-07-04.
7. rd edition).
8. Schwamborn D., Gerhold, T., and Heinrich R. (2006), The DLR tau-code: recent applications in research and industry, European Conference on Computational Fluid Dynamics ECCOMAS CFD 2006, in P. Wesseling, E. Oñate, J. Périaux (Eds), TU Delft, The Netherlands, 2006.
9. Rudnik R., Rossow C.-C. and von Geyr H. (2002), Numerical simulation of engine/airframe integration for high-bypass engines, Aerospace Science and Technology, 6 (1), pp. 31-42.
10. Scheimpflug T. (1904), Improved Method and Apparatus for the Systematic Alteration or Distortion of Plane Pictures and Images by Means of Lenses and Mirrors for Photography and for other purposes, Patent specification No. 1196, Great Britain.
11. Vollmers H., Puffert-Meissner W. and Schröder A. (2006), Analysis of PIV Flow Field Measurements behind the ALVAST-Model in High-Lift Configuration, In: Rath H.-J., Holze C., Heinemann H.-J., Henke R. and Hönlinger H. (Ed.), Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), Springer-Verlag, Berlin, 92, pp. 17-24.
12. T.F. Brooks; T.H. Hodgson (1981) "Trailing Edge Noise Prediction from Measured Surface Pressures". In Journal of Sound and Vibration, Volume 78, No. 1, 1981, pp. 69 -117.
13. R. Ewert; W. Schröder (2003) "Acoustic Perturbation Equations based on Flow Decomposition via Source Filtering". In Journal of Computational Physics, Volume 188, 2003, pp. 365-398.
14. R. Ewert; W. Schröder (2004) "On the Simulation of Trailing Edge Noise with a Hybrid LES/APE Method". In Journal of Sound and Vibration, Volume 270, 2004, pp. 509-524.
15. J.E. Ffowcs Williams; L.H. Hall (1970) "Aerodynamic Sound Generation by Turbulent Flow in the Vicinity of a Scattering Half Plane". In J. Fluid Mech., Vol. 40, 1970, pp. 657-670.
16. M. Herr; W. Dobrzynski (2005) "Experimental Investigations in Low-Noise Trailing-Edge Design". In AIAA-Journal, Volume 43, No. 6, 2005, pp. 1167-1175.
17. M.S. Howe (1978) "A Review of the Theory of Trailing Edge Noise". In Journal of Sound and Vibration, Volume 61, No. 3, 1978, pp. 437-465.
18. W. Möhring (1979) "Modelling Low Mach Number Noise". In Mechanics of Sound Generation in Flows, edited by E. A. Müller, Springer, 1979.
19. A. Powell (1964) "Theory of Vortex Sound". In Journal of the Acoustical Society of America, Volume 36, No 1, 1964, pp. 177-195.
20. C. Tam; J. Webb (1993) "Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics". In J. Comp. Phys., Volume 107, 1993, pp. 262-281.