Joint prediction of aircraft gas turbine engine axial flow compressor off-design performance and surge line based on the expanded method of generalized functions
Crossref DOI link: https://doi.org/10.3103/S106879981403012X
Published Online: 2015-01-10
Published Print: 2014-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mikhailova, A. B.
Akhmedzyanov, D. A.
Akhmetov, Yu. M.
Mikhailov, A. E.
Text and Data Mining valid from 2014-07-01