A theoretical/empirical model for rolling delta wings with vortex breakdown

16th AIAA Applied Aerodynamics Conference

Volumn , Issue , 1998, Pages 299-308

  Myatt, James H ^a   Arena, Andrew S ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Oklahoma State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; PLANFORMS; VORTEX FLOW;

COMPLICATED FLOW; DELTA WINGS; FIRST ORDER; ROLL ANGLE; ROLLING MOMENTS; SLENDER BODIES; VORTEX BREAKDOWN; VORTEX BREAKDOWN LOCATION;

DELTA WING AIRCRAFT;

EID: 84983189170     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2527     Document Type: Conference Paper

References (14)

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2. Brown, C. E. and Michael, W. H., Jr., "On Slender Delta Wings with Leading-Edge Separation," NACA Technical Note 3430, Apr., 1955.
3. Mangier, K. W. and Smith, J. H. B., "Calculation of the Flow past Slender Delta Wings with Leading Edge Separation," RAE Report No. Aero. 2593, May, 1957.
4. Cohen, M. J. and Nimri, D., "Aerodynamics of Slender Rolling Wings at Incidence in Separated Flow," AIAA Journal, Vol. 14, No. 7, 1976, pp. 886-893.
5. Arena, A. S., Jr., An Experimental and Computational Investigation of Slender Wings Undergoing Wing Rock, Ph. D. Dissertation, Dept. of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, 1992, Chaps. 5-6.
6. Arena, A. S., Jr. and Nelson, R. C., "A Discrete Vortex Model for Predicting Wing Rock of Slender Wings," AIAA Paper 92-4497, 1992.
7. Myatt, J. H., Modeling the Rolling Moment on the 65-Degree Delta Wing for Rolling Motions at High Angle of Attack, Ph. D. Dissertation, Dept. of Aeronautics and Astronautics, Stanford University, Stanford, CA, 1997, Chap. 8.
8. Milne-Thomson, L. M., Theoretical Aerodynamics, 4th ed., St Martin's Press, NY, 1966.
9. Katz, J. and Plotkin, A., Low-Speed Aerodynamics From Wing Theory to Panel Methods, McGraw-Hill, Inc., NY, 1991.
10. Bisplinghoff, R. L, Ashley, H. and Halfman, R. L., Aeroelasticity, Addison-Wesley Publishing Co., Inc., Cambridge, MA, 1955, pp. 251-261.
11. Wentz, W. H., Jr. and Kohlman, D. L., "Vortex Breakdown on Slender Sharp-Edged Wings," Journal of Aircraft, Vol. 8, No. 3, Mar., 1971, pp. 156-161.
12. Hanff, E. S. and Huang, X. Z., "Roll-Induced Cross-Loads on a Delta Wing at High Incidence," AIAA Paper 91-3223, Sept., 1991.
13. Greenwell, D. I. and Wood, N. J., "Determination of Vortex Burst Location on Delta Wings from Surface Pressure Measurements," AIAA Journal, Vol. 30, No. 11, Nov., 1992, pp. 2736-2739.
14. Hsia, A. H., Myatt, J. H. and Jenkins, J. E., "Nonlinear and Unsteady Aerodynamic Responses of a Rolling 65-Degree Delta Wing," AIAA Paper 93-3682, Aug., 1993.