Lift-to-drag ratio losses due to longitudinal trimming in joined wing configuration at cruise flight mode

2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD) Pub Date : 2017-10-01 DOI:10.1109/APUAVD.2017.8308773

K. Predachenko, O. Lemko

引用次数: 1

Abstract

This paper present Lift-to-Drag ratio losses estimation procedure for several configuration of Joined Wing UAVs at cruise flight mode, that actual at initial design stage for comparison or optimization purpose.

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在巡航飞行模式下，联合翼结构纵向修整造成的升阻比损失

本文给出了几种组合翼无人机在巡航飞行模式下的升阻比损失估算方法，并在初始设计阶段进行了比较和优化。

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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来源期刊

2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)

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