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Engineering method integrated with CAD-system for optimizing the horizontal empennage parameters of the maneuverable aircraft
| Authors: Romanova T.N., Paschenko O.B., Gavrilova N.Yu., Schetinin G.A. | Published: 08.04.2016 |
| Published in issue: #2(107)/2016 | |
| DOI: 10.18698/0236-3933-2016-2-40-52 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Innovation Technologies in Aerospace Activity | |
| Keywords: CAD-system, CAE-system, multi-objective optimization, horizontal aircraft empennage, moment of the horizontal empennage | |