Rapid Method of Predicting the Subsonic Flutter Stability of AGTE Axial-Flow Compressor Blade Cascades. Part 1. Physical Backgrounds of the Method
Crossref DOI link: https://doi.org/10.1007/s11223-019-00063-y
Published Online: 2019-05-30
Published Print: 2019-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Stel’makh, A. L.
Zinkovskii, A. P.
Kabannik, S. N.
Text and Data Mining valid from 2019-03-01
Version of Record valid from 2019-03-01
Article History
Received: 7 December 2017
First Online: 30 May 2019