Results of a parametric aeroelastic stability analysis of a generic X-wing aircraft
暂无分享,去创建一个
Jessica A. Woods | Michael G. Gilbert | Terrence A. Weisshaar | T. Weisshaar | J. A. Woods | M. Gilbert
[1] J. P. Giesing,et al. Subsonic Unsteady Aerodynamics for General Configurations. Part 1. Volume I. Direct Application of the Nonplanar Doublet-Lattice Method , 1971 .
[2] J. R. Banerjee,et al. Flutter characteristics of high aspect ratio tailless aircraft , 1984 .
[4] T. A. Weisshaar,et al. Flutter of forward swept wings, analyses and tests , 1982 .
[5] J. R. Newsom,et al. A method for obtaining reduced-order control laws for high-order systems using optimization techniques , 1981 .
[6] D. Gimmestad. A preliminary divergence and flutter evaluation of an X-wing aircraft , 1981 .
[7] I. C. Cheeseman,et al. The Application of Circulation Control by Blowing to Helicopter Rotors , 1967, The Journal of the Royal Aeronautical Society.
[8] Inderjit Chopra,et al. Flutter of circulation control wings , 1988 .
[9] W. M. Adams,et al. A Digital Program for Calculating the Interaction Between Flexible Structures, Unsteady Aerodynamics and Active Controls , 1979 .