Rapid method of Predicting the Subsonic Flutter Stability of AGTE Axial-Flow Compressor Blade Cascades. Part 2. Mathematical Implementation of Method and its Potentional Application
Crossref DOI link: https://doi.org/10.1007/s11223-019-00117-1
Published Online: 2019-12-05
Published Print: 2019-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zinkovskii, A. P.
Kabannik, S. N.
Stel’makh, A. L.
Text and Data Mining valid from 2019-09-01
Version of Record valid from 2019-09-01
Article History
Received: 7 December 2017
First Online: 5 December 2019