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

Q3 Earth and Planetary Sciences

Aerospace Systems Pub Date : 2023-07-17 DOI:10.1007/s42401-023-00240-7

Gulnar Resulkulyeva, Sergey Serebryansky

引用次数: 0

Abstract

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.

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基于回归分析确定超音速行政客机机身结构重量的方法

本文介绍了制造超音速行政客机的主要项目以及超音速行政客机重量分析的特点。从重量分析的角度考虑了高温运行条件下结构的资源和强度问题。在回归分析的基础上，提出了计算超音速行政客机机身第一近似质量的模型。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Aerospace Systems Social Sciences-Social Sciences (miscellaneous)

CiteScore

1.80

自引率

0.00%

发文量

期刊介绍： Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion