Synthesis of basic structural design of aircraft GTE based on genetic algorithms
Anatoliy I. Belousov, A. Yu. Sapozhnikov · Russian Aeronautics · 2015
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.