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- W3083345503 abstract "This thesis discusses a comparison of the differences in aerodynamic performance of wings designed with elliptical and bell-shaped lift distributions. The method uses a Standard Cirrus sailplane wing with a lift distribution associated with the induced drag benefits of an elliptical distribution (span efficiency = 0.96) as the basis of comparison. The Standard Cirrus is a standard class sailplane with 15-meter wingspan that was designed by Schempp-Hirth in 1969. This sailplane wing was modeled and analyzed in XFLR5, then validated against existing wind tunnel airfoil data, and Standard Cirrus flight test data. The root bending moment of the baseline wing was determined and used as the primary constraint in the design of two wings with bell-shaped lift distribution. These wings were modeled in XFLR5 by adjusting chord length and geometric twist respectively, and then they were studied using fixed speed lifting line analysis. Steady state cruise conditions for the Standard Cirrus sailplane were taken from the flight test data and applied for the analysis." @default.
- W3083345503 created "2020-09-11" @default.
- W3083345503 creator A5057135092 @default.
- W3083345503 date "2023-08-02" @default.
- W3083345503 modified "2023-09-27" @default.
- W3083345503 title "A Study of the Standard Cirrus Wing Lift Distribution Versus Bell Shaped Lift Distribution" @default.
- W3083345503 doi "https://doi.org/10.15368/theses.2020.59" @default.
- W3083345503 hasPublicationYear "2023" @default.
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