Аuthors
Kuprikov M. Y.1*,
Dolgov O. S.**,
Kuprikov N. M.2***
1. ,
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: kuprikov@mai.ru
**e-mail: dolgov@mai.ru
***e-mail: nkuprikov@gmail.com
Abstract
In report is widely descripted a new approach to the analysis of inertia-moments of aircraft design, based on solving the inverse problem and identified the boundaries of the existing methods for determining the inertia-moments of perspective aircraft, a new direction to develop new methods for determining the inertia-moments of the aircraft is suggested.
Keywords:
aircraft design, inertia-moments inner layout, volume-weight layout