Open AccessОСОБЕННОСТИ ИНТЕГРИРОВАННОГО ПРОЕКТИРОВАНИЯ ГРАЖДАНСКИХ ЛЕГКИХ САМОЛЕТОВ С ТУРБОВИНТОВЫМИ ДВИГАТЕЛЯМИ НА ЭТАПЕ ПРЕДВАРИТЕЛЬНОГО ПРОЕКТИРОВАНИЯ
Author(s) -
А. Г. Гребеников,
А. М. Гуменный,
Л. Ю. Буйвал
Publication year - 2018
Publication title -
otkrytye informacionnye i kompʹûternye integrirovannye tehnologii
Language(s) - English
Resource type - Journals
eISSN - 2663-2411
pISSN - 2071-1077
DOI - 10.32620/oikit.2018.81.02
Subject(s) - turboprop , aeronautics , range (aeronautics) , software , computer science , engineering , aerospace engineering , programming language
The analysis of changes in the parameters and characteristics of civilian light aircraft. New ways of improving its quality, improving tactical, technical and flight characteristics to meet a wide range of areas of its using have been proposed. The limits of change are established and the statistical ranges of parameters and characteristics of civilian light aircraft are refined. Recommendations are given on the method for determining the take-off mass of a civilian light aircraft with turboprop engines at the preliminary design stage in accordance with the optimality criterion - the minimum take-off mass. The features of the software package and its approbation during the development of KhAI-90 civil light aircraft preliminary project are described.