Synthesis of basic structural design of aircraft GTE based on genetic algorithms

Synthesis of basic structural design of aircraft GTE based on genetic algorithms

A functional IDEF0-model of conceptual design of an aircraft gas turbine engine was developed. By an example of selecting a structural design of two-rotor gas turbine engine, we present the structured analysis of the engine and describe the operation of the genetic algorithm.

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Veröffentlicht in:Russian aeronautics 2015-04, Vol.58 (2), p.199-204
Hauptverfasser: Belousov, A. I., Sapozhnikov, A. Yu
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Design and Development
Automotive Engineering
Engineering
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Zusammenfassung:A functional IDEF0-model of conceptual design of an aircraft gas turbine engine was developed. By an example of selecting a structural design of two-rotor gas turbine engine, we present the structured analysis of the engine and describe the operation of the genetic algorithm.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799815020105