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The paper explores the design issues of controllable rescue parachute wing for UAS (Unmanned Aircraft System). The main part of the paper designs a prototype of an aerodynamically defined rescue parachute wing. On top of that, the XFLR5 and fwDesign software are used to design the canopy and its characteristics. The results are mainly available through a summary table containing basic parameters of the prototype, graphs exploring the aerodynamic characteristics and other exhibits of copious amounts of images illustrating dimensions, shape, structure, and the layout of individual construction parts.
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Škultéty et al. (2018) studied this question.
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