Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage
Crossref DOI link: https://doi.org/10.3103/S1068799819010239
Published Online: 2019-06-10
Published Print: 2019-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Grigor’ev, V. A.
Zagrebel’nyi, A. O.
Text and Data Mining valid from 2019-01-01
Version of Record valid from 2019-01-01
Article History
Received: 22 July 2015
Revised: 16 May 2016
First Online: 10 June 2019