Methods for determining the weight of a supersonic passenger administrative aircraft fuselage structure based on regression analysis

被引：0
|
作者：
Resulkulyeva G. [1 ]
Serebryansky S. [1 ]
机构：
[1] Moscow Aviation Institute (National Research University), Moscow
来源：
Aerospace Systems | 2024年 / 7卷 / 01期
关键词：
Prediction of the weight of the fuselage structure; Regression analysis; Weight design; Weight perfection of the supersonic passenger administrative aircraft;
D O I：
10.1007/s42401-023-00240-7
中图分类号：
学科分类号：
摘要：
This paper describes the main projects for the creation of supersonic administrative aircraft and the features of the weight analysis of supersonic passenger administrative aircraft. The question of the resource and strength of the structure in operating conditions at high temperatures is considered from the point of view of weight analysis. A model is proposed for calculating the mass of the supersonic passenger administrative aircraft fuselage in the first approximation based on regression analysis. © Shanghai Jiao Tong University 2023.
引用
收藏
页码：159 / 166
页数：7
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