Experimental investigation of aerodynamic performance of a small UAV with a telescopic wing

2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD) Pub Date : 2013-10-01 DOI:10.1109/APUAVD.2013.6705272

I. Kryvokhatko, V. Sukhov

引用次数: 4

Abstract

Telescopic wing is the mechanism aimed to increase lift-to-drag ratio of aircraft or UAV by increasing wing aspect ratio. In previous study theoretical mathematical models of the aerodynamic performance of the telescopic wing UAV for low Reynolds number were developed. The present study investigates these characteristics experimentally.

查看原文本刊更多论文

小型无人机伸缩翼气动性能实验研究

伸缩翼是通过增大机翼展弦比来提高飞机或无人机的升阻比的机构。在以往的研究中，建立了低雷诺数伸缩翼无人机气动性能的理论数学模型。本研究对这些特性进行了实验研究。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文求助全文

来源期刊

2013 IEEE 2nd International Conference Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD)

自引率

0.00%

发文量