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LIST OF REFERENCES<br />

1. Bunton, R. W., and Denegri, C. M., “Limit Cycle Oscillation Characteristics <strong>of</strong> Fighter<br />

Aircraft,” Journal <strong>of</strong> Aircraft, Vol. 37, No. 5, 2000, pp. 916-918.<br />

2. Pasiliao, C. L., and Dubben, J. A., “Analysis <strong>of</strong> CFD Pressure Coefficients on the F-16<br />

Wing Associated with Limit Cycle Oscillations,” AIAA Paper 2008-0409, January 2008.<br />

3. Pasiliao, C. L., and Dubben, J. A., “Determination <strong>of</strong> Flow Field Characteristics <strong>of</strong> F-16<br />

Wing Associated with Limit Cycle Oscillations Using CFD,” Proceedings <strong>of</strong> the NATO<br />

RTO Symposium AVT-152 on Limit-Cycle Oscillations and other Amplitude-Limited,<br />

Self-Excited Vibrations, N<strong>or</strong>way, May 2008.<br />

4. Pasiliao, C. L., and Dubben, J. A., “CFD Based Determination <strong>of</strong> Transonic Flow Field<br />

Characteristics <strong>of</strong> F-16 Wing Associated with LCO,” AIAA-2009-1084, January 2009.<br />

5. Pasiliao, C. L., and Dubben, J. A., “Transient Analysis <strong>of</strong> Transonic Flow Field<br />

Characteristics <strong>of</strong> F-16 Wing Associated with LCO,” Abstract Accepted to Proceedings<br />

<strong>of</strong> the IFASD Conference, Seattle, WA, June 2009.<br />

6. Bisplingh<strong>of</strong>f, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Mineola, NY: Dover<br />

Publications, Inc., 1955.<br />

7. Denegri, C. M., Jr., and Cutchins, M. A., “Evaluation <strong>of</strong> Classical Flutter Analysis f<strong>or</strong> the<br />

Prediction <strong>of</strong> Limit Cycle Oscillations,” AIAA Paper 1997-1021, April 1997.<br />

8. Denegri, C. M., Jr., “Fundamentals <strong>of</strong> Flutter Engineering,” Air F<strong>or</strong>ce SEEK EAGLE<br />

Office Training Materials, Eglin AFB, FL, June 2003.<br />

9. Hassig, H. J., “An Approximate True Damping Solution <strong>of</strong> the Flutter Equation by<br />

Determinant Iteration,” AIAA Journal <strong>of</strong> Aircraft, Vol. 3, No. 11, 1971, pp. 885-889.<br />

10. Ward, D. T., and Strganac, T. W., Introduction to Flight Test Engineering, 2 nd Ed.,<br />

Dubuque, IA: Kendall/Hunt Company, 2001, pp. 218-250.<br />

11. N<strong>or</strong>ton, W. J., “Limit Cycle Oscillation and Flight Flutter Testing,” 21 st Annual<br />

Symposium Proceedings, Society <strong>of</strong> Flight Test Engineers, Lancaster, CA, 1990, pp. 3.4-<br />

1–3.4-12.<br />

12. Denegri, C. M., Jr., “Limit Cycle Oscillation Flight Test Results <strong>of</strong> a Fighter with<br />

External St<strong>or</strong>es,” Journal <strong>of</strong> Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.<br />

13. Denegri, C. M., Jr., “Limit Cycle Oscillation Flight Test Results <strong>of</strong> a Fighter with<br />

External St<strong>or</strong>es,” AIAA Paper 2000-1394, April 2000.<br />

14. Dreyer, C. A., and Shoch, D. L., “F-16 Flutter Testing at Eglin Air F<strong>or</strong>ce Base,” AIAA<br />

Paper 86-9819, April 1986.<br />

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