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 Stanford University   (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)

1. Sobak, M. and Schiff, L. B., "Aerodynamic Mathematical Modeling-Basic Concepts," AGARD Lecture Series No. 114, Paper 1, March 1981.
2. Tobak, M., Chapman, G. T., and Ünal, A., "Modeling aerodynamic discontinuities and onset of chaos in flight dynamical systems," annales des telecommunications, Tome 42, no. 56, 1987, pp. 300-314.
3. Truong, K. V. and Tobak, M., "Indicial Response Approach Derived from Navier-Stokes Equations Part 1-Time-Invariant Equilibrium State," NASA, TM-102856, Moffet Field, CA, Oct. 1990.
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.
6. Jenkins, J. E., Myatt, J. H., and Hanff, E. S, "Body-Axis Rolling Motion Critical States of a 65-Degree Delta Wing," Journal of Aircraft, Vol. 33, No. 2, 1996, pp 268-278.
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.
11. Ogata, K., Modern Control Engineering, Prentice-Hall, Inc., Englewood Cliffs, N. J., 1970, pp. 495-497.