变形翼在Hydra Technologies UAS-S4上的应用

IF 0.7 4区计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS

Modeling Identification and Control Pub Date : 2017-02-21 DOI:10.2316/P.2016.848-048

M. Segui, O. S. Gabor, A. Koreanschi, R. Botez

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引用次数: 4

摘要

本文介绍了在Hydra Technologies公司的UAS S4 Ehecatl上进行的变形机翼研究的空气动力学结果。只考虑了飞机的巡航阶段(恒定高度和恒定速度)。从气动的角度来看，通过计算和比较变形机翼和原始机翼的纵向气动系数(阻力和升力)来强调它们之间的差异。利用旋涡格点法对龙卷风的气动特性进行了计算。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Morphing wing application on Hydra Technologies UAS-S4

This paper presents the aerodynamic results of a morphing wing study performed on the UAS S4 Ehecatl from Hydra Technologies. Only the cruise phase of the aircraft was considered (constant altitude and constant speed). The difference, from an aerodynamic point of view, between the morphing wing and the original wing was emphasized by computing and comparing their longitudinal aerodynamic coefficients (drag and lift). The computation of the aerodynamic characteristics was done using tornado with the Vortex Lattice Method.

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来源期刊

Modeling Identification and Control 工程技术-计算机：控制论

CiteScore

3.30

自引率

0.00%

发文量

审稿时长

>12 weeks

期刊介绍： The aim of MIC is to present Nordic research activities in the field of modeling, identification and control to the international scientific community. Historically, the articles published in MIC presented the results of research carried out in Norway, or sponsored primarily by a Norwegian institution. Since 2009 the journal also accepts papers from the other Nordic countries.