Experimental study on controlling wake vortex in water towing tank

ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities

Volumn , Issue , 2003, Pages 214-223

  Bao, Feng ^a   Vollmers, Heinrich ^a   Mattner, Hartmut ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ASPECT RATIO; ATTENUATION; FLOW VISUALIZATION; TURBULENCE; VELOCITY MEASUREMENT; WAKES; WATER TANKS; WINGS;

PARTICLE IMAGE VELOCIMETRY (PIV); SELF-DESTRUCTIVE MECHANISM;

VORTEX FLOW;

EID: 1642475447     PISSN: 07302010     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Brandon, Jay M., Jordan, Frank L., Jr., and Stuever, Robert A., 1997: "Application of Wind Tunnel Free-Flight Technique for Wake Vortex Encounters" NASA Technical Paper 3672, November 1997
2. Brooke Benjamin, T., 1962: "Theory of the vortex breakdown phenomenon", J.F.M. Vol.4, part4, pp.539-629
3. Crow, S.C. 1970: "Stability Theory for a Pair of Trailing Vortices", AIAA Journal, VOL. 8, No. 12, phenomenon.2172-2179
4. Denecke, H., Kreplin, H.-P., 2002: "Kraftmessungen mit einer Piezo-Waage am Wirbelschleppen-Prinzipmodel im Wasserschleppkanal", IB 224-2002 A02
5. Fabre, D., Jacquin, L. & Loof, A., 2002: "Optimal perturbations in a four-vortex aircraft wake in counter-rotating configuration", JFM, Vol.451, pp.319-328
6. Gerz, T., Holzäpfel, F., Darracq, D.,2002: "Commercial Aircraft Wake Vortices", Progr. Aerosp. Sci. Vol.38, pp.181-208
7. th International Symposium on Flow Visualization
8. th International Symposium on Particle Image Velocimetry, Göttingen, Germany, Sept. 17-19, 2001
9. Olsen, John H., 1970: "Flow-field Visualization in Aircraft Wake Vortex Research", Aircraft Wake Turbulence and its Detection, Proceedings of a Symposium on Aircraft Wake Turbulence, Seattle, Washington September 1-3, 1970, pp.455-472
10. Raffel, M., Willert, C., Kompenhans, J. 1996: "Particle Image Velocimetry", ISBN 3-540-63683-8, Springer-Verlag
11. Rossow, V.J., 1999: "Lift-Generated Vortex Wakes of Subsonic Transport Aircraft", Progress in Aerospace Science, 35(1999) 507-660
12. Stuff, R. 2002, "Premature breakdown of vortices as a consequence of the Rayleigh-Ludwieg instability", EuroMech Colloquium No 433, 2002, Aachen
13. Speijker, L.J.P. Blom, H.A.P. Kos, J., 1999: "Assessment of Wake Vortex Safety to Evaluate Separation Distances", Research fro Safety in Civil Aviation, Paris, October 21-22, 1999
14. Williamson, C.H.K. and Cerretelli, C., 2002: "Merging of co-rotating vortices", in Proc. Euromech Colloquium 433, Dynamics of Trailing Vortices, RWTH Aachen, Germany, March 2002