The problem of determining the design parameters of the gas turbine engine for a helicopter
Crossref DOI link: https://doi.org/10.3103/S106879981403009X
Published Online: 2015-01-10
Published Print: 2014-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Grigor’ev, V. A.
Zagrebel’nyi, A. O.
Text and Data Mining valid from 2014-07-01