Effects of angle of attack on nonlinear flutter of a delta wing

AIAA journal

Volumn 39, Issue 1, 2001, Pages 15-21

  Tang, Deman ^a   Dowell, Earl H ^a  

^a DUKE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; OSCILLATIONS; SUBSONIC FLOW; VORTEX FLOW; WINGS;

KARMAN PLATE THEORY; LIMIT CYCLE OSCILLATIONS (LCO);

FLIGHT DYNAMICS;

EID: 0034833242     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1296     Document Type: Article

References (5)

1. Doggett, R. V., and Solstmann, D. L., "Some Low-Speed Flutter Characteristics of Simple Low-Aspect-Ratio Delta Wing Models," NASA TM 101547, Jan. 1989.
2. Tang, D. M., Dowell, E. H., and Hall, K. C., "Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow," AIAA Journal, Vol. 37, No. 3, 1999, pp. 364-371.
3. Tang, D. M., Henry, J. K., and Dowell, E. H., "Limit Cycle Oscillations of Delta Wing Models in Low Subsonic Flow," AIAA Journal, Vol. 37, No. 11, 1999, pp. 1355-1362.
4. Hall, K. C., "Eigenanalysis of Unsteady Flows About Airfoils, Cascades, and Wings," AIAA Journal, Vol. 32, No. 12, 1994, pp. 2426-2432.
5. Bunton, R. W., and Denegri, C. M., Jr., "Limit Cycle Oscillation Characteristics of Fighter Aircraft," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 916-918.