A study of wale effect on the flow over a delta wing

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 156-166

  Verhaagen, N G ^a   Houtman, E M ^a   Verhelst, J M ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FLOW FIELDS; REYNOLDS NUMBER; VORTEX FLOW; WIND TUNNELS;

CROSSSECTIONAL GEOMETRY; EXISTING TUNNEL; LEADING-EDGE VORTICES; LOW-SPEED WIND TUNNEL; THREE-DIMENSIONAL EULER EQUATIONS; TUNNEL WALL; WALL EFFECTS; WING SURFACE;

DELTA WING AIRCRAFT;

EID: 84964290921     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Verhaagen, N.G., Meeder, J.P. and Verhelst, J.M., "Boundary Layer Effects on the Flow of a Leading Edge Vortex, " AIAA-93-3463-CP, Monterey, August 1993.
2. Nelson, R.C. and Visser, K. D., "Breaking Down the Delta Wing Vortex, " Vortex Flow Dynamics, AGARD-CP-494, Paper 21, Scheveningen, October 1990.
3. Garner, H.C. and Rogers, E.W.E., "Subsonic Wind-Tunnel Wall Corrections, " AGAR Dograph 109, 1966.
4. Fnnk, N.T., "Computational Study of Wind-Tunnel Wall Effects on the Flow Field around Delta Wings, " AIAA-87-2420, 1987.
5. Houtman, E. M. and Bannink, W.J., "Experimental and Numerical Investigation of the Vortex Flow over a Delta Wing at Transonic Speed, " Vortex Flow Dynamics, AGARD-CP-494, Paper 5, Scheveningen, October 1990.
6. Houtman, E.M., Bakker, P.G., de Vries, E. and van den Berg, J.C., "Modelling of Separation using Euler Methods, " TUD Report LR-776, October 1994.
7. Karou, A., "Separated Vortex Flow over Slender Wings between Side Walls, Theoretical and Experimental Investigation, " TUD Report LR-300, August 1980.
8. Kwong, CM. and Myring, D.F., "Fusiform-body Separated Flow Field Calculation using Euler and Boundary Layer Methods, " In: RAeS Conference, The Prediction and Exploitation of Separated Flow, 1989.
9. Verhaagen, N.G., "An Experimental Investigation of the Vortex Flow over Delta and Double- Double-Delta Wings at Low Speed, " Aerodynamics of Vortical Type Flows in Three Dimensions, AGARD-CP-342, Paper 7, Rotterdam, April 1983.
10. Visser, K.D. and Washburn, A.E., "Transition Behaviour on Flat Plate Delta Wings, " AIAA-94-1850, Colorado Springs, June 1994.
11. Washburn, A.E. and Visser, K.D., "Evolution of Vortical Structures in the Shear layer of Delta Wings, " AIAA-94-2317, Colorado Springs, June 1994.
12. Ding, Z., Shih, C. and Lourenco, L., "Leading Edge Vortices of a Delta Wing Flow Field - A PIV Study, " AIAA-95-0652, Reno, January 1995.
13. Visbal, M.R., "Computational and Physical Aspects of Vortex Breakdown on Delta Wings, " AIAA-95-0585, Reno, January 1995.