Abstract
References 1Norton,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. 2Cunningham, A. M., Jr., “Practical Problems: Airplanes,” Unsteady Transonic Aerodynamics, AIAA, Washington, DC, 1989, Chap. 3, pp. 83, 84. 3Denegri, 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. 4Airplane Strength and Rigidity—Vibration, Flutter, and Divergence, MIL-SPEC MIL-A-8870B, 20 May 1987, p. 3. 5Dreyer, C. A., and Shoch, D. L., “F-16 Flutter Testing at EglinAir Force Base,” AIAA Paper 86-9819, April 1986.
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