Modeling the rolling 65-degree delta wing with critical state encounters

22nd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1997, Pages 411-421

  Myatt, James H ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CRITICAL CURRENT DENSITY (SUPERCONDUCTIVITY); FLOW FIELDS; STATE SPACE METHODS; TIME MEASUREMENT; TOPOLOGY; VORTEX FLOW;

AERODYNAMIC MODELING; LAPLACE DOMAINS; MULTIPLE TIME SCALE; SHORT TIME SCALE; STATE SPACE FORM; TRANSIENT EFFECT; VORTEX BREAKDOWN; VORTEX BREAKDOWN LOCATION;

DELTA WING AIRCRAFT;

EID: 84983134062     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Skow, A. M., "Agility as a Contributor to Design Balance," Journal of Aircraft, Vol. 29, No. 1, 1992, pp. 34-46.
2. 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.
3. 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.
4. Tobak, M. and Chapman, G. T., "Nonlinear Problems in Flight Dynamics Involving Aerodynamic Bifurcations," Unsteady Aerodynamics—Fundamentals and Applications to Aircraft Dynamics, AG ARD CP-386, Paper 25, May, 1985.
5. Huang, X. Z., Hanff, E. S., Jenkins, J. E., and Addington, G. A., "Leading-Edge Vortex Behavior on a 65° Delta Wing Oscillating in Roll," AIAA Paper 943507, Aug., 1994.
6. 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, No. 10, 1954, pp. 690-694.
7. Youngren, H. H., Bouchard, E. E., and Coopersmith, R. M., "Quadrilateral Element Panel Method: Users Manual," Ver. 3. 2, Lockheed LR 30563, Burbank, CA, 1984.
8. 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.
9. Ogata, K., Modern Control Engineering, Prentice-Hall, Inc., Englewood Cliffs, N. J., 1970, pp. 28-42, 221-225, 375-376, 495-496, 675-678.
10. Montgomery, D. C. and Peck, E., Introduction to Linear Regression Analysis, 2nd ed., John Wiley & Sons, Inc., NY, 1992, pp. 7-16, 159-160.
11. Kirk, D. E., Optimal Control Theory: An Introduction, Prentice-Hall Inc., Englewood Cliffs, N. J., 1970, pp. 331-333.
12. Jenkins, J. E., "The Nonlinear Indicial Response: Vis-a-Vis Roll-Rate Induced Camber Effects," AIAA Paper 94-3458, Aug., 1994.