A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis

A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis

This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Russian aeronautics 2018, Vol.61 (1), p.78-83
Hauptverfasser: Rybakov, V. N., Kuz’michev, V. S., Tkachenko, A. Yu, Krupenich, I. N.
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Theory
Aircraft components
Automotive Engineering
Engineering
Gas turbine engines
Optimization
Process parameters
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:This paper describes a method for multicriteria optimization of parameters for both the engine core and engine family with modeling the engine operation as a part of aircraft system.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799818010129