An algebraic model for bypass transition in turbomachinery boundary layer flows

Sławomir Kubacki , Eric Dick

Abstract

n/a
Author Sławomir Kubacki (FPAE / IAAM)
Sławomir Kubacki,,
- The Institute of Aeronautics and Applied Mechanics
, Eric Dick - [Universiteit Gent]
Eric Dick,,
-
-
Journal seriesInternational Journal of Heat and Fluid Flow, ISSN 0142-727X, (A 40 pkt)
Issue year2016
Vol58
Pages68-83
Publication size in sheets0.75
ASJC Classification1507 Fluid Flow and Transfer Processes; 2210 Mechanical Engineering; 3104 Condensed Matter Physics
DOIDOI:10.1016/j.ijheatfluidflow.2016.01.001
URL www.elsevier.com/locate/ijheatfluidflow
Languageen angielski
Score (nominal)40
ScoreMinisterial score = 35.0, 06-09-2019, ArticleFromJournal
Ministerial score (2013-2016) = 40.0, 06-09-2019, ArticleFromJournal
Publication indicators WoS Citations = 13; Scopus Citations = 14; Scopus SNIP (Source Normalised Impact per Paper): 2016 = 1.746; WoS Impact Factor: 2016 = 1.873 (2) - 2016=2.304 (5)
Citation count*20 (2019-11-18)
Cite
Share Share

Get link to the record


* presented citation count is obtained through Internet information analysis and it is close to the number calculated by the Publish or Perish system.
Back
Confirmation
Are you sure?