Development of a user-friendly interface for conceptual shape design of subsonic airplanes and gliders
The conceptual design enables initial estimation of the characteristics of aircraft and gliders, such as shape, drag, power, and range, and some low-fidelity approaches and analytical formulae were proposed and applied to develop a user-friendly interface, which provides an interactive mode and allows using arbitrary s...
I. Nesteruk, Oleksii Dorozhkin
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