3Bennett R M. An overview of recent development in computational aeroelasticity [ R] . AIAA, 1998 : 1 - 14.
4Suciu E. Msc/nastran flutter analyses of T-tails including horizontal stabilizer static lift effects and T-tail transonic dip [C]. The 1996 Msc/Nastran World User's Conference. Newport Beach. CA, 1996.
5Quarantal G, Riccil S, Scottil A, et al. Aeroelastic investigation and design improvements on a three surface transport airplane [ R]. XVIII Congresso Nazionale Aidaa. Settembre, 2005, Volterra(PI) : 19 - 22.
6Chuban V D. Influence of angle of attack and stabilizer deflection on tempennage flutter [J].Journal of Aircraft, 2005, 42 ( 1 ) : 264 - 268.
9Land N S, Fox A G. An experimental investigation of the effects of mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail [M]. NasaTvD-924,1961.