Gust Alleviation of a Large Aircraft with a Passive Twist Wingtip
نویسندگان
چکیده
منابع مشابه
Gust Alleviation of a Large Aircraft with a Passive Twist Wingtip
This paper presents an investigation into the gust response and wing structure load alleviation of a 200-seater aircraft by employing a passive twist wingtip (PTWT). The research was divided into three stages. The first stage was the design and analysis of the baseline aircraft, including aerodynamic analysis, structural design using the finite element (FE) method and flutter analysis to meet t...
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ژورنال
عنوان ژورنال: Aerospace
سال: 2015
ISSN: 2226-4310
DOI: 10.3390/aerospace2020135