A nonlinear indicial response model for the rolling 65-degree delta wing

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 364-374

  Myall, James H ^a   Jenkins, Jerry E ^b  

^a Department of Aeronautics and Astronautics Department of Mechanical Engineering and Industrial for Computational and Mathematical Engineering   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRITICAL CURRENT DENSITY (SUPERCONDUCTIVITY); VORTEX FLOW;

AXIS INCLINATION; INVISCID FLOWS; MODEL PARAMETERS; NONLINEAR INDICIAL RESPONSE; ROLLING MOMENTS; SUPERPOSITION INTEGRAL; VORTEX BREAKDOWN; VORTICAL FLOWS;

DELTA WING AIRCRAFT;

EID: 84983187966     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

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4. Jenkins, J. E. and Hanff, E. S., "Highlights of the IAR/WL Delta Wing Program," AIAA Workshop on Delta Wings: Unsteady Aerodynamics and Modeling, Aug. 1995.
5. 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.
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7. Jobe, C. E., Hsia, A. H., Jenkins, J. E., and Addington, G. A., "Critical States and Flow Structure on a 65-Deg Delta Wing," Journal of Aircraft, Vol. 33, No. 2, 1996, pp. 347-352.
8. Huang, X. Z., Hanff, E. S., Jenkins, J. E., and Addington, G., "Leading-Edge Vortex Behavior on a 65° Delta Wing Oscillating in Roll," AIAA Paper 943507, Aug. 1994.
9. Brown, C. E. and Michael, Jr., W. H., "Effect of Leading-Edge Separation on the Lift of a Delta Wing," Journal of the Aeronautical Sciences, Vol. 21, 1954, pp. 690-694.
10. Youngren, H. H., Bouchard, E. E., and Coopersmith, R. M., "Quadrilateral Element Panel Method: Users Manual Ver. 3. 2," Lockheed, 1984.
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