Effectiveness of flow control for alleviation of twin-Tail buffet

AIAA and SAE World Aviation Conference, 1998

Volumn , Issue , 1998, Pages

  Sheta, Essam F ^a   Kandil, Osama A ^a   Yang, Zhi ^a  

^a Old Dominion University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ASPECT RATIO; COMPUTATION THEORY; COMPUTATIONAL METHODS; DELTA WING AIRCRAFT; FLEXIBLE WINGS; FLOW CONTROL; REYNOLDS NUMBER; SWEPT WINGS; VORTEX FLOW;

ACTIVE FLOW CONTROL; AEROELASTIC RESPONSE; FREESTREAM MACH NUMBER; HIGH ANGLES OF ATTACK; LEADING-EDGE VORTICES; MULTIDISCIPLINARY PROBLEMS; SEPARATION DISTANCES; SHARP-EDGED DELTA WING;

AEROELASTICITY;

EID: 85086948632     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-5501     Document Type: Conference Paper

References (11)

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3. Lee, B. and Brown, D., "Wind Tunnel Studies of F/A-18 Tail Buffet, " AIAA 90-1432, 1990.
4. Cole, S. R., Moss, S. W. and Dogget, R. V. Jr., "Some Buffet Response Characteristics of a Twin-Vertical-Tail Configuration, " NASA TM-102749, October 1990.
5. Washburn, A. E., Jenkins, L. N. and Ferman, M. A., "Experimental Investigation of Vortex-Fin Interaction, " AIAA 93-0050, AIAA 31st ASM, Reno, NV, January 1993.
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8. Sheta, E. F. and Kandil, 0. A., "Effect of Configuration Pitching Motion on Twin Tail Buffet Response, " AIAA-98-0520, 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 12-15, 1998.
9. Wong, G. S., Rock, S. M., Wood, N. J. and Roberts, L., "Active Control of Wing Rock Using Tangential Leading-Edge Blowing, " Journal of Aircraft, Vol. 31, No. 3, May- June 1994.
10. Hummel, D. "On the Vortex Formation over A Slender Wing at Large Angles of Incidence, " AGARD-CP-247, Oct. 1978.
11. Sheta, E. F., "Computational Investigation and Validation of Twin-Tail Buffet Response Including Dynamics and Control, " Ph.D. Dissertation, Old Dominion University, May 1998.