2020
DOI: 10.3233/atde200097
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Verification of Flutter Method for the Purposes of Building a Very Flexible Wing Generative Model

Abstract: First step of aircraft design is calculation of initial parameters, based on assumptions determining flight parameters which designed aircraft should meet. During these calculations, it is possible to pre-detect structure instability called a flutter. These calculations are made based on the geometric parameters assumed in the first conceptual drawings of the flying vehicle. Assumed masses and speeds allow for preliminary analysis of forces acting on the structure. The next step is to determine the displacemen… Show more

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“…This article details aspects of the development of a solar-powered UAV which is designed to be able to fly in the stratosphere-TwinStratos (TS) UAV [35][36][37]. The goal of this research was to obtain an understanding of the laminated solar cells used in the first, smaller prototype of TS (Figure 1).…”
mentioning
confidence: 99%
“…This article details aspects of the development of a solar-powered UAV which is designed to be able to fly in the stratosphere-TwinStratos (TS) UAV [35][36][37]. The goal of this research was to obtain an understanding of the laminated solar cells used in the first, smaller prototype of TS (Figure 1).…”
mentioning
confidence: 99%