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- W2002102505 abstract "A STUDY of the effects of mass and stiffness changes on the flutter degradation of optimized wings is presented in this paper. The wings were optimized for weight with constraints on strength, displacement, and flutter speed. The mass and stiffness changes are representative of battle damage. The structural box is idealized by finite elements consisting of membranes, shear panels, and bar elements. The aerodynamic force matrix is generated by incompressible strip theory. Five damage models involving two wing boxes are included. The effect of damage on aerodynamic flow is not treated." @default.
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- W2002102505 date "1980-12-01" @default.
- W2002102505 modified "2023-09-27" @default.
- W2002102505 title "Flutter Speed Degradation of Damaged, Optimized Flight Vehicles" @default.
- W2002102505 cites W2172261643 @default.
- W2002102505 doi "https://doi.org/10.2514/3.57972" @default.
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