Journal of Applied and Computational Mechanics
Moment-Inertial Factor as a Criterion for Assessing the Dimension of an Aircraft
Document Type : Research Paper
Authors
1 Department of Engineering Graphics, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation
2 Institute of General Engineering Education, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation
3 Department of Perspective Materials and Technologies of Aerospace Designation, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation
4 Science-Information Center “Polar Initiative”, Moscow Aviation Institute (National Research University), 4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation
Abstract
The study aims to compare the characteristics of the moment-inertial schemes of two aircrafts – a mainline aircraft of a normal aerodynamic scheme and an aircraft made according to the flying wing scheme, to improve their flight performance. The study uses the method of successive approximations using relative masses (when determining m0), the formula of A. Mozhaisky, an artificial method consisting of the layout of the aircraft oriented to the virtual center of mass. Design studies at the modern level of scientific and technical development have confirmed the relevance of using the proposed methods of forming a moment-inertial appearance for promising long-haul aircraft of large passenger capacity.
Keywords
Main Subjects
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