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- W2379654872 abstract "The mechanical analysis and the trimming were performed for a novel near space aircraft which uses the variation in wind speed at high altitude to control its flight path.The flight principle of the novel aircraft was analyzed,and its parameters were determined.Because of the differences in the mechanical characteristics and relative airspeeds of the aircraft components,the forces applied on the components were analyzed separately,and a force balance equation set was established,in which a tether was analyzed in 3D space by using a segmenting analytical method.Finally,for each component,the simultaneous trimming calculation of equation set was performed by using an iterative method,and the spatial profiles of the tether were plotted.The computational results show that the wind speed difference in the stratosphere can be used to control the flight path of aircraft with the result that its energy consumption is significantly decreased." @default.
- W2379654872 created "2016-06-24" @default.
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- W2379654872 date "2008-01-01" @default.
- W2379654872 modified "2023-09-26" @default.
- W2379654872 title "Mechanical Analysis and Trimming of an Energy-saving Near Space Aircraft" @default.
- W2379654872 hasPublicationYear "2008" @default.
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