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- W1993229047 abstract "Joined-wing aircraft employ tandem wings having positive and negative sweep and dihedral, arranged to form diamond shapes in both plan and front views. An optimization method was applied to study the effects of joined-wing geometry parameters on structural weight. The lightest wings were obtained by increasing dihedral and taper ratio, decreasing sweep and span, increasing fraction of airfoil chord occupied by structural box, and locating the joint inboard of the front wing tip." @default.
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- W1993229047 date "1988-12-01" @default.
- W1993229047 modified "2023-09-26" @default.
- W1993229047 title "Parametric weight evaluation of joined wings by structural optimization" @default.
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- W1993229047 doi "https://doi.org/10.2514/3.45714" @default.
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