An algebraic model for bypass transition in turbomachinery boundary layer flows

Sławomir Kubacki , Eric Dick

Abstract

n/a
Author Sławomir Kubacki ITLMS
Sławomir Kubacki,,
- The Institute of Aeronautics and Applied Mechanics
, Eric Dick
Eric Dick,,
-
Journal seriesInternational Journal of Heat and Fluid Flow, ISSN 0142-727X
Issue year2016
Vol58
Pages68-83
Publication size in sheets0.75
DOIDOI:10.1016/j.ijheatfluidflow.2016.01.001
URL www.elsevier.com/locate/ijheatfluidflow
Languageen angielski
Score (nominal)40
ScoreMinisterial score = 35.0, 28-11-2017, ArticleFromJournal
Ministerial score (2013-2016) = 40.0, 28-11-2017, ArticleFromJournal
Publication indicators WoS Impact Factor: 2016 = 1.873 (2) - 2016=2.304 (5)
Citation count*9 (2018-07-15)
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* presented citation count is obtained through Internet information analysis and it is close to the number calculated by the Publish or Perish system.
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