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- W4283204928 abstract "This work outlines the simulation of the stability and control characteristics of box-wing aircraft, conducted in X-Plane. The box-wing is a non-planar lifting system that distributes lift equally between two primary lifting surfaces, which are joined laterally at the tips by endplates. The system theoretically exhibits minimum induced drag for a given span. The gap, stagger and decalage between the primary lifting surfaces, as well as the significant additional control surface placement options, requires careful simulation to ensure suitable stability and control characteristics. Modeling of the box-wing aircraft model is achieved using PlaneMaker, and the assumptions and control surface placement decisions are discussed. Flight-testing was undertaken using X-Plane. Handling characteristics flight tests were conducted for takeoff and cruise, using a qualified civilian pilot, to determine the implications under operational conditions. The flight-testing included the determination of stall speed, stall characteristics, as well as the lateral, longitudinal, and normal axis stability." @default.
- W4283204928 created "2022-06-22" @default.
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- W4283204928 date "2022-06-20" @default.
- W4283204928 modified "2023-09-23" @default.
- W4283204928 title "Simulation of the Stability and Control Characteristics of a Box-Wing Aircraft" @default.
- W4283204928 cites W2157289187 @default.
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- W4283204928 doi "https://doi.org/10.2514/6.2022-3846" @default.
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