DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT

机译：新一代联动翼飞机低速引风机的设计与优化

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摘要

The Paper describes the process of design of apusher ducted fan propulsion system for anunmanned aerial vehicle MOSUPS designed ina joined wing configuration.Aerodynamic design followed by real timeresults obtained from tests in a wind tunnel havebeen described. Everything is summarized withconclusions showing what has been learnt fromthe whole design and research.

机译：该文件描述了设计的过程推进器风管推进系统无人机MOSUPS设计于连接的机翼配置。空气动力学设计，然后实时从风洞测试中获得的结果有被描述。一切都总结为结论表明从中学到了什么整个设计与研究。

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来源
《Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences》|2014年|1-5|共5页
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作者
Krzysztof Bogdański; Witold Krusz; Mirosław Rodzewicz; Mariusz Rutkowski;
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原文格式 PDF
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关键词
Ducted Fan; UAV;

机译：风管风扇;;无人机;

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4. DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT [C] . Krzysztof Bogdański, Witold Krusz, Miros?aw Rodzewicz, Congress of the International Council of the Aeronautical Sciences . 2014

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DESIGN AND OPTIMIZATION OF LOW SPEED DUCTED FAN FOR A NEW GENERATION OF JOINED WING AIRCRAFT

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