ERRATUM - Geometrically Exact. Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams
LAUNCH VEHICLE AND MISSILE (LV-M) TECHNOLOGY - Tension Buckling in Shear-Flexible Composite Beams
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
ERRATA - Geometrically Exact, Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams
LATERAL-TORSIONAL FLUTTER OF A DEEP CANTILEVER LOADED BY A LATERAL FOLLOWER FORCE AT THE TIP
Finite Element Solution of Nonlinear Intrinsic Equations for Curved Composite Beams
Application of the Variational-Asymptotical Method to Laminated Composite Plates
Control Variables for Finite Element Solution of Missile Trajectory Optimization