Limit cycle oscillation characteristics of fighter aircraft

Journal of Aircraft

Volumn 37, Issue 5, 2000, Pages 916-918

  Bunton, Robert W ^a   Denegri Jr , Charles M ^b  

^a US Naval Air Warfare Center   (United States)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; DYNAMIC RESPONSE; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); FUSELAGES; OSCILLATIONS; SUBSONIC AERODYNAMICS; TRANSONIC AERODYNAMICS; WINGS;

AIRCRAFT RESPONSE CHARACTERISTICS; LIMIT CYCLE OSCILLATIONS;

FIGHTER AIRCRAFT;

EID: 0034273920     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2690     Document Type: Article

References (5)

1. Norton, W. J., "Limit Cycle Oscillation and Flight Flutter Testing," Proceedings of the 21st Annual Symposium, Society of Flight Test Engineers, Lancaster, CA, 1990, pp. 3.4-1-3.4-12.
2. Cunningham, A. M., Jr., "Practical Problems: Airplanes," Unsteady Transonic Aerodynamics, AIAA, Washington, DC, 1989, Chap. 3, pp. 83, 84.
3. Denegri, C. M., Jr., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.
4. Airplane Strength and Rigidity - Vibration, Flutter, and Divergence, MIL-SPEC MIL-A-8870B, 20 May 1987, p. 3.
5. Dreyer, C. A., and Shoch, D. L., "F-16 Flutter Testing at Eglin Air Force Base," AIAA Paper 86-9819, April 1986.