Abstract 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.
Synthesis of basic structural design of aircraft GTE based on genetic algorithms
Russian Aeronautics (Iz VUZ) ; 58 , 2 ; 199-204
2015-04-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Synthesis of basic structural design of aircraft GTE based on genetic algorithms
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