Publications

Rotorcraft

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Publication Name File Size
High-Fidelity Aeroservoelastic Predictive Analysis Capability Incorporating Rigid Body Dynamics
P. M. Thompson, Ph.D., B. P. Danowsky, C. Farhat, Ph.D., T. Lieu, Ph.D., J. Lechniak, and C. Harris, presented at AIAA Atmospheric Flight Mechanics Conference, Portland, OR, 8-11 August 2011. (STI-P-766)
917.0 KiB
Incorporation of Feedback Control into a High-Fidelity Aeroservoelastic Fighter Aircraft Model
B. P. Danowsky, P. M. Thompson, Ph.D., C. Farhat, Ph.D., T. Lieu, Ph.D., C. Harris, and J. Lechniak, Journal of Aircraft, vol. 47,no. 4, pp. 1274-1282, 2010. (AIAA 2009-5708, STI-P-735)
 1.7 MiB
Aeroservoelastic Predictive Analysis Capability
P. M. Thompson, Ph.D., D. H. Klyde, C. Farhat, Ph.D., and C. Harris, Ph.D., "Aeroservoelastic Predictive Analysis Capability," presented at AIAA Atmospheric Flight Mechanics Conference, Hilton Head, SC, 20-23 August 2007. (AIAA 2007-6716, STI-P-697)
 664.4 KiB
Evaluation of Aeroelastic Uncertainty Analysis Methods
B. P. Danowsky, J. P. Chrstos, Ph.D., D. H. Klyde, C. Farhat, Ph.D., and M. J. Brenner, "Evaluation of Aeroelastic Uncertainty Analysis Methods," Journal of Aircraft, vol. 47,no. 4, pp. 1266-1273, 2010. (AIAA 2008-6371, STI-P-712J)
 494.6 KiB
Residualization of an Aircraft Linear Aeroelastic Reduced Order Model to Obtain Static Stability Derivatives
B. P. Danowsky, P. M. Thompson, Ph.D., C. Farhat, Ph.D., and C. Harris, Ph.D., "Residualization of an Aircraft Linear Aeroelastic Reduced Order Model to Obtain Static Stability Derivatives," presented at AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, Hawaii, 18 - 21 August 2008. (AIAA 2008-6370, STI-P-711)
 115.5 KiB
Using Describing Functions for Limit-Cycle-Oscillation Analysis Applied to Aeroservoelastic Models with Free-Play
B. P. Danowsky, P. M. Thompson, Ph.D., and S. Kukreja, Ph.D., presented at 48th AIAA Aerospace Sciences Meeting, Orlando, FL, January 4-7, 2010. (AIAA 2010-492, STI-P-736)
 336.0 KiB