Vortex breakdown location over 65° delta wings empiricism and experiment

16th AIAA Applied Aerodynamics Conference

Volumn , Issue , 1998, Pages 288-298

  Jobe, Charles E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DELTA WING AIRCRAFT; FORECASTING; GEOMETRY; LOCATION; NAVIER STOKES EQUATIONS;

EXPERIMENTAL DETERMINATION; FLOW CONTROL STRATEGY; GEOMETRIC VARIATIONS; LEADING-EDGE BEVELS; LEADING-EDGE VORTICES; NAVIER-STOKES COMPUTATIONS; PREDICTION METHODS; VORTEX BREAKDOWN LOCATION;

VORTEX FLOW;

EID: 84982318352     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2526     Document Type: Conference Paper

References (30)

1. Huang, X. Z., and Hanff, E. S., "Unsteady Behavior of Spiral Leading-Edge Vortex Breakdown," AIAA Paper 96-3408, July, 1996.
2. Huang, X. Z., and Hanff, E. S., "Prediction of Normal Force on a Delta Wing Rolling at High Incidence," AIAA 93-3686, Aug., 1993.
3. Cipolla, K. M., "Structure of the Flow Past a Delta Wing with Variations in Roll Angle," Ph. D. Dissertation, Lehigh University, May, 1996.
4. Earnshaw, P. B., "Measurements of Vortex-Breakdown Position at Low Speed on a Series of Sharp-Edged Symmetrical Models," ARC C. P. No. 828, Nov., 1964.
5. Earnshaw, P. B., and Lawford, J. A., "Low-Speed Wind-Tunnel Experiments on a Series of Sharp-Edged Delta Wings," ARC R. &M. No. 3424, Mar., 1964.
6. Guglieri, G., and Quagliotti, F. B., "Experimental Investigation of Vortex Dynamics on Delta Wings," AIAA Paper 92-2731, June, 1992.
7. Guglieri, G., Onorato, M., and Quagliotti, F. B., "Vortex Breakdown Study on a 65° Delta Wing Tested in Static and Dynamic Conditions," ICAS 92-4. 10. 2, ICAS Proceedings, Sept., 1992, pp. 2072-2081.
8. Lambourne, N. C., and Bryer, D. W., "The Bursting of Leading-Edge Vortices-Some Observations and Discussion of the Phenomena," ARC R. &M. No. 3282, Apr., 1961.
9. Lowson, M. V., and Riley, A. J., "Vortex Breakdown Control by Delta Wing Geometry," J. Aircraft, Vol. 32, No. 4, 1995, pp. 832-838. Also see AIAA Paper 94-3487 Aug. 1994.
10. Panton, R. L., "Effects of a Contoured Apex on Vortex Breakdown," J. Aircraft, Vol. 27, No. 3, 1993, pp. 285-288. Also see AIAA Paper 89-0193, Jan 1989.
11. Pelletier, A., "An Experimental Investigation of Vortex Breakdown on Slender Delta-Wing Planforms," MS Thesis, University of Notre Dame, April, 1994.
12. Pelletier, A., and Nelson, R. C., "An Experimental Study of Static and Dynamic Vortex Breakdown on Slender Delta Wing Planforms," AIAA Paper 94-1879, June, 1994.
13. Skow, A. M., and Erickson, G. E., "Modern Fighter Aircraft Design for High-Angle-of-Attack Maneuvering," AGARD-LS-121, "High Angle-of-Attack Aerodynamics," Dec., 1982, pp. 4-1 to 4-59.
14. Erickson, G. E., "Vortex Flow Correlation," AFWAL-TR-80-3143, Jan., 1981.
15. Thompson, D. H., "A Water Tunnel Study of Vortex Breakdown Over Wings with Highly Swept Leading Edges," Note ARL/A. 356, May 1975, Australian Defence Scientific Service.
16. Traub, L. W., "Simple Prediction Method for Location of Vortex Breakdown on Delta Wings," J. Aircraft, Vol. 33, No. 2, 1996, pp. 452-454.
17. Wentz, W. H., Jr., and Kohlman, D. L., "Vortex Breakdown on Slender Sharp-Edged Wings," AIAA Paper 69-778, July, 1969. Also see J. Aircraft, Vol. 8, No. 3, 1971, pp. 156-161.
18. Wentz, W. H., Jr., and Kohlman, D. L., "Wind Tunnel Investigations of Vortex Breakdown on Slender Sharp-Edged Wings," Univ. of Kansas Report FRL 68-013, Nov., 1968 (NASA CR 98737 also N69-14762).
19. Huang, X. Z., Sun, Y. Z. and Hanff, E. S., "Further Investigations of Leading-Edge Vortex Breakdown Over Delta Wings," AIAA Paper 97-2263, June 1997.
20. Huang, X. Z., Sun, Y. Z. and Hanff, E. S., "Circulation Criterion to Predict Leading-Edge Vortex Breakdown Over Delta Wings," AIAA Paper 97-2265, June 1997.
21. Traub, L. W., "Prediction of Vortex Breakdown and Longitudinal Characteristics of Swept Slender Planforms," J. Aircraft, Vol. 34, No. 3, May-June 1997, pp. 353-359.
22. Verhaagen, N. G., "Effect of Sideslip on the Flow over a 65-deg Delta Wing; Preliminary Report," Delft Univ. of Technology, The Netherlands, Dec., 1997.
23. Addington, G. A., "The Role of Flow Field Structure in Determining the Aerodynamic Response of a Delta Wing," Ph. D. Dissertation, University of Notre Dame, Notre Dame, Indiana, April, 1998.
24. Chaderjian, N., and Schiff, L., "Navier-Stokes Prediction of a Delta Wing in Roll with Vortex Breakdown," AIAA Paper 93-3495, Aug., 1993.
25. Gordnier, R. E., "Numerical Simulation of a 65 Degree Delta-Wing Flowfield," J. Aircraft, Vol. 34, No. 4, 1997, pp. 492-499. Also see AIAA Paper 95-0082, Jan. 1995.
26. Gursul, L, "Unsteady Flow Phenomena over Delta Wings at High Angle of Attack," AIAA Journal, Vol. 32, No. 2, 1994, pp. 225-231.
27. Hemsch, M. J., and Luckring, J. M., "Connection Between Leading-Edge Sweep, Vortex Lift, and Vortex Strength for Delta Wings," J. Aircraft, Vol. 27, No. 5, pp. 473-475.
28. Visser, K. D., and Nelson, R. C., "Measurements of Circulation and Vorticity in the Leading-Edge Vortex of a Delta Wing," AIAA Journal, Vol. 31, No. 1, 1993, pp. 104-111.
29. Jumper, E. J., Nelson, R. C. and Cheung, K., "A Simple Criterion for Vortex Breakdown," AIAA-93-0866, Jan., 1993.
30. Visser, K. D., and Washburn, A. E., "Transition Behavior on Flat Plate Delta Wings," AIAA-94-1850-CP, June, 1994.