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- W4285738427 abstract "This research develops and analyses a general aviation plane. A preliminary representation of the eventual product is used to start the design process for an airplane. Based on a drawing, a design mission profile is utilized to determine the weight. A more advanced approach is used to estimate weight, which employs calculated performance criteria to produce a more exact weight estimate. The wing design has been demonstrated to be a feasible alternative for a similar general aviation aircraft. When traveling through air or other fluids, a wing is a type of fin that provides lift. Airfoils may be observed on the wings, which have a streamlined cross-section, as a result of this. The lift created by a wing is compared to the drag generated by it to determine its aerodynamic efficiency." @default.
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- W4285738427 date "2022-06-01" @default.
- W4285738427 modified "2023-09-27" @default.
- W4285738427 title "Design And Analysis of Aircraft Wing." @default.
- W4285738427 doi "https://doi.org/10.47893/gret.2022.1133" @default.
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