A skin design method of variable camber wing trailing edge
نویسندگان
چکیده
As an important part of the wing, skin deformation accuracy directly affect aerodynamic performance aircraft in different environments. Based on idea easy processing and deformation, a method for designing variable section thickness trailing edge camber wings is proposed. In this paper, firstly, length each segment 3~8 segments are optimized. Then results compared analyzed. Finally, correctness design effectiveness verified by using stacked experiment.
منابع مشابه
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ژورنال
عنوان ژورنال: Xibei gongye daxue xuebao
سال: 2023
ISSN: ['1000-2758', '2609-7125']
DOI: https://doi.org/10.1051/jnwpu/20234120329