Reduced-order aeroservoelastic model with an unsteady aerodynamic eigen formulation

AIAA Journal

Volumn 35, Issue 6, 1997, Pages 1087-1088

  Kim, Taehyoun ^a,d,e,f   Nam, Changho ^b,f,g   Kim, Youdan ^c,f,g  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b Hankuk Aviation University   (South Korea)

^c Seoul National University   (South Korea)

^d Computational Mechanics Center ^*  (United States)

^e BOEING COMPANY   (United States)

^f AIAA   (United States)

^g Dept of Aero and Mech Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; MODELLING-MATHEMATICAL;

EID: 0030760618     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.201     Document Type: Article

References (3)

1. Dowell, E. H., "Eigenmode Analysis in Unsteady Aerodynamics: Reduced-Order Models," AIAA Journal, Vol. 34, No. 8, 1996, pp. 1578-1583.
2. Hall, K. C., "Eigenanalysis of Unsteady Flows About Airfoils, Cascades, and Wings," AIAA Journal, Vol. 32, No. 12, 1994, pp. 2426-2432.
3. Mueller, G. S., and Adeniyi, V. O., "Optimal Output Feedback by Gradient Methods with Optimal Stepsize Adjustment," Proceedings of IEE, Control and Science, Vol. 126, No. 10, 1979, pp. 1005-1007.