Control of twin-tail buffet responses using normal leading-edge blowing

18th Applied Aerodynamics Conference

Volumn , Issue , 2000, Pages

  Sheta, Essam F ^a  

^a CFD RESEARCH CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; BENDING (FORMING);

BENDING DEFLECTION; HIGH PRESSURE; POWER REQUIREMENT; ROOT BENDING MOMENT; TWIN-TAILS; VORTICAL FLOWS;

WINGS;

EID: 85085402482     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4227     Document Type: Conference Paper

References (14)

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2. Wood, N. J. and Roberts, L., "Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing," Journal of Aircraft, Vol. 25, No. 3, March 1988, pp. 236-243.
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8. Sheta, E. F., Harrand, V. J., and Huttsell, L. J., "Active Vortical Flow Control for Alleviation of Twin-Tail Buffet of Generic Fighter Aircraft," AIAA 2000-0906, AIAA 38th ASM, January 2000.
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