Critical-state transients for a rolling 65-degree delta wing

Journal of Aircraft

Volumn 34, Issue 3, 1997, Pages 380-386

  Grismer, Deborah S ^a,b,c   Jenkins, Jerry E ^a,b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Building 146   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; MANEUVERABILITY;

CRITICAL STATE TRANSIENTS; DELTA WINGS; HARMONIC ROLLING MOTIONS; MACH NUMBER; STEADY STATE VALUE;

WINGS;

EID: 0031143926     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2180     Document Type: Article

References (17)

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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. Huang, X. Z., and Hanff, E. S., "Roll Rate Induced Camber Effect on Delta Wing Leading-Edge Vortex Breakdown," AIAA Paper 95-1793, June 1995.
4. Ericsson, L., and Hanff, E. S., "Further Analysis of High-Rate Rolling Experiments of a 65-Deg Delta Wing," Journal of Aircraft, Vol. 31, No. 6, 1994, pp. 1350-1357.
5. 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 94-3507, Aug. 1994.
6. Huang, X. Z., and Hanff, E. S., "Prediction of Normal Force on a Delta Wing Rolling at High Incidence," AIAA Paper 93-3686, Aug. 1993.
7. Hsia, A. H., Myatt, J. H., and Jenkins, J. E., "Nonlinear and Unsteady Aerodynamic Responses of a Rolling 65-Delta Wing," AIAA Paper 93-3682, Aug. 1993.
8. Addington, G., and Jenkins, J., "Flow Visualization of a Rolling Delta Wing and Its Pertinence to the Nonlinear Indicial Response Model," AIAA Paper 93-3469, Aug. 1993.
9. Huang, X. Z., and Hanff, E. S., "Prediction of Leading-Edge Vortex Breakdown on a Delta Wing Oscillating in Roll," AIAA Paper 92-2677, June 1992.
10. Hanff, E. S., and Huang, X. Z., "Roll-Induced Cross-Loads on a Delta Wing at High Incidence," AIAA Paper 91-3223, Sept. 1991.
11. Hanff, E. S., and Jenkins, S. B., "Large-Amplitude High-Rate Rolling Experiments on a Delta and Double Delta Wing," AIAA Paper 90-0224, Jan. 1990.
12. Hanff, E. S., Kapoor, K., Anstey, C. R., and Prini, A., "Large-Amplitude High-Rate Roll Oscillation System for the Measurement of Non-Linear Loads," AIAA Paper 90-1426, June 1990.
13. Jenkins, J. E., and Hanff, E. S., "Highlights of the IAR/WL Delta Wing Program," AIAA Workshop on Delta Wings: Unsteady Aerodynamics and Modeling, Atmospheric Flight Mechanics Conf., Aug. 1995.
14. Youngren, H. H., Bouchard, E. E., and Coopersmith, R. M., "Quadrilateral Element Panel Method: User's Manual Ver. 3.2," Lockheed-California Co., Burbank, CA, 1984.
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16. Tobak, M., Chapman, G. T., and Unal, A., "Modeling Aerodynamic Discontinuities and Onset of Chaos in Flight Dynamical Systems," Annales des Telecommunications, Tome 42, Nos. 5, 6, 1987, pp. 300-314; also NASA TM-89420, Dec. 1986.
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