Vortical substructures in the shear layers forming leading-edge vortices

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Mitchell, Anthony ^a   Molton, Pascal ^b   Barberis, Didier ^b   Délery, Jean ^b  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; DELTA WING AIRCRAFT; DOPPLER EFFECT; FLOW FIELDS; REYNOLDS NUMBER; SHEAR FLOW; WIND TUNNELS;

CHORD-BASED REYNOLDS NUMBER; FLOW FIELD MEASUREMENT; HIGH ANGLES OF ATTACK; LASER DOPPLER VELOCIMETRY; LEADING-EDGE VORTICES; MEASUREMENT TECHNIQUES; SUBSONIC WIND TUNNELS; VORTEX BREAKDOWN LOCATION;

VORTEX FLOW;

EID: 85067316959     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2424     Document Type: Conference Paper

References (27)

1. Délery, J., Physics of Vortical Flows, AIAA Journal of Aircraft, Vol. 29, No. 5, Sept-Oct 1992, pp. 856-876.
2. Werlé, H., Sur l'éclatement des tourbillons, ONERA Note Technique No. 175, Châtillon, France, Nov. 1971.
3. Werlé, H., Quelques résultats expérimentaux sur les ailes en fleche, aux faibles vitesses, obtenus en tunnel hydrodynamique, La Recherche Aéronautique, No. 33, 1953.
4. Hall, M.G., Vortex Breakdown, Annual Review of Fluid Mechanics, Vol. 4, 1972, pp. 195-218.
5. Leibovich, S., The Structure of Vortex Breakdown, Annual Review of Fluid Mechanics, Vol. 10, 1978, pp. 221-46.
6. Sarpkaya, T. On Stationary and Traveling Vortex Breakdowns, Journal of Fluid Mechanics, Vol. 45, Part 3, 1971, pp. 545-559.
7. Nelson, R.C., Unsteady Aerodynamics of Slender Wings, Aircraft Dynamics at High Angles of Attack: Experiments and Modeling, AGARD-R-776, 1991, pp. 11 to 1-26.
8. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1995.
9. Délery, J., Aspects of Vortex Breakdown, Progress in Aerospace Sciences, Vol. 30, 1994, pp. 1-59.
10. Squire, H.B., Jones, J.G., Stanbrook, A., An Experimental Investigation of the Characteristics of some Plane and Cambered 65 Deg Delta Wings at Mach Numbers from 0.7 to 2.0, ARC,iíáMNo. 3305, 1961.
11. Gad-El-Hak, M., Blackwelder, R.F., The Discrete Vortices from a Delta Wing, AIAA Journal, Vol. 23, No. 6, June 1985, pp. 961-962.
12. Payne, F.M., Ng, T.T., Nelson, R.C., Schiff, L.B., Visualization and Wake Surveys of Vortical Flow over a Delta Wing, AIAA Journal, Vol. 26, No. 2, Feb. 1988, pp. 137-143.
13. nd AIAA Shear Flow Conference, Tempe, AZ, March 1989.
14. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1989.
15. Molton, P., Etude experiméntale de l'écaltement tourbillonnaire sur aile delta en écoulement incompressible: characterisation du champ externe, Onera RT 53/1147AN, 1992.
16. Mitchell, A.M., Caractérisation et controle de l'éclatement tourbillonnaire sur une aile delta aux hautes incidences, Ph.D. These, Université de Paris 6, Departement de Mécanique, Juillet 2000.
17. Drazin, P.G., Reed, W.H., Hydrodynamic Stability, Cambridge University Press, 1981.
18. Ho, CM., Huerre, P., Perturbed Free Shear Layer, Annual Review of Fluid Mechanics, Vol. 16, 1984, pp. 365-424.
19. Gordnier, R.E., Computation of a Kelvin-Helmholtz Instability for Delta Wing Vortex Flows, WL-TR-91-3098, Flight Dynamics Directorate, Wright Laboratory, Wright-Paterson AFB, OH, Nov. 1991.
20. th AIAA Applied Aerodynamics Conference, Monterey, CA, Aug. 1993.
21. th AIAA Fluid Dynamics Conference, Colorado Springs, CO, June 1994.
22. rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1995.
23. Honkan, A., Andreopoulos, J., Instantaneous Three-Dimensional Vorticity Measurements in Vortical Flow over a Delta Wing, AIAA Journal, Vol. 35, No. 10, Oct. 1997, pp. 1612-1620.
24. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1998.
25. th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1988.
26. th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 1998.
27. Barberis, D., Test Cases for CFD Validation, Onera TP No. 1993-161, Châtillon, France, 1993.