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- W2023444583 abstract "A computational method developed to provide a transonic analysis for upper/lower surface wing-tip mounted winglets is described. Winglets with arbitrary planform, cant and toe angle, and airfoil section can be modeled. The embedded grid approach provides high flow field resolution and the required geometric flexibility. In particular, coupled Cartesian/cylindrical grid systems are used to model the complex geometry presented by canted upper/lower surface winglets. A new rotated difference scheme is introduced in order to maintain the stability of the small-disturbance formulation in the presence of large spanwise velocities. Wing and winglet viscous effects are modeled using a two-dimensional 'strip' boundary layer analysis. Correlations with wind tunnel and flight test data for three transport configurations are included." @default.
- W2023444583 created "2016-06-24" @default.
- W2023444583 creator A5091113570 @default.
- W2023444583 date "1984-01-09" @default.
- W2023444583 modified "2023-09-23" @default.
- W2023444583 title "Transonic analysis of canted winglets" @default.
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- W2023444583 doi "https://doi.org/10.2514/6.1984-302" @default.
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