Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/38320
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dc.contributor.authorKulyk, Mykolaen
dc.contributor.authorDmitriev, Sergiyen
dc.contributor.authorYakushenko, Oleksandren
dc.contributor.authorPopov, Oleksandren
dc.date.accessioned2019-04-06T14:02:58Z-
dc.date.available2019-04-06T14:02:58Z-
dc.date.issued2013-05-
dc.identifier.issn1648-7788-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/38320-
dc.description.abstractA method of obtaining test and training data sets has been developed. 弻ese sets are intended for train- ing a static neural network to recognise individual and double defects in the air-gas path units of a gas-turbine engine. 弻ese data are obtained by using operational process parameters of the air-gas path of a bypass turbofan engine. 弻e method allows sets that can project some changes in the technical conditions of a gas-turbine engine to be received, taking into account errors that occur in the measurement of the gas-dynamic parameters of the air-gas path. 弻e op- eration of the engine in a wide range of modes should also be taken into accounten
dc.language.isoenuk_UA
dc.publisherAviation. Taylor&Francisen
dc.relation.ispartofseries17(2) 2013;-
dc.subjectgas-turbine engineen
dc.subjectair-gas pathen
dc.subjectmathematical model of operational processen
dc.subjectneural networken
dc.titleMethod of formulating input parameters of neural network for diagnosing gas-turbine enginesen
dc.typeArticleen
dc.specialityAviationen
Appears in Collections:Наукові статті кафедри авіаційних двигунів (НОВА)

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