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dc.contributor.author | Adgamov R. | |
dc.contributor.author | Dmitriev S. | |
dc.contributor.author | Khairullin A. | |
dc.date.accessioned | 2018-09-18T20:18:06Z | |
dc.date.available | 2018-09-18T20:18:06Z | |
dc.date.issued | 2012 | |
dc.identifier.issn | 1068-7998 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/138478 | |
dc.description.abstract | The quality control system for an aircraft engine that is continuously developed in the life cycle stages is considered. Main quality indicators and their control methodology are analyzed. The computer-aided tests are substantiated as part of the quality control system and their generalized technological process structure and its construction methodology are proposed. © 2012 Allerton Press, Inc. | |
dc.relation.ispartofseries | Russian Aeronautics | |
dc.subject | computer-aided test system | |
dc.subject | quality control system | |
dc.subject | quality indicators | |
dc.title | Computer-aided tests in the quality control system of aircraft engines | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 1 | |
dc.relation.ispartofseries-volume | 55 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 101 | |
dc.source.id | SCOPUS10687998-2012-55-1-SID84861686429 |