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- W215544964 abstract "A method is presented for calculating the aerodynamic forces on a moncylane wing, taking into account the elastic twisting of the wing due to these forces. The lift distribution along the span is calculated by the formulas of Amstutz as a function of the geometrical characteristics of the wing and of the twist at stations 60 and 90 percent of the semispan. The twist for a given lift distribution is calculated by means of influence lines. As a numerical example, the forces on a Swiss military D.2V airplane are calculated. Comparisons with the strip method and with the ordinary stress-analysis method are also given." @default.
- W215544964 created "2016-06-24" @default.
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- W215544964 date "1935-01-01" @default.
- W215544964 modified "2023-09-27" @default.
- W215544964 title "Calculations of the Effect of Wing Twist on the Air Forces Acting on a Monoplane Wing" @default.
- W215544964 hasPublicationYear "1935" @default.
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