Abstract The ways of obtaining the performance of separate nozzles for turbofan engines are presented using the method of experiment planning, namely, the method of the Greco-Latin squares and the technique of approximation of multivariate functions.
Nozzle performance study in a turbofan engine with a high bypass ratio using the method of experiment planning
Russian Aeronautics (Iz VUZ) ; 58 , 2 ; 237-243
2015-04-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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