About the GPPS Journal
Aims and Scope
International Advisory Board
Editorial Board
Contact
Journal Home
Submissions
Editorial Processes
Submission and Manuscript Guidelines
Fees
Reviewer Guidelines
Permissions Guide for Authors
Indexing and Archiving
GPPS Editorial Policies
CrossMark, Correction and Retraction Policy
Journal issues
Terms & Conditions
Cookie Policy
Copyright Notice
Privacy Policy
GPPS Copyright and Licences
GPPS Licence Agreement
About the GPPS Journal
Aims and Scope
International Advisory Board
Editorial Board
Contact
Journal Home
Submissions
Editorial Processes
Submission and Manuscript Guidelines
Fees
Reviewer Guidelines
Permissions Guide for Authors
Indexing and Archiving
GPPS Editorial Policies
CrossMark, Correction and Retraction Policy
Journal issues
Terms & Conditions
Cookie Policy
Copyright Notice
Privacy Policy
GPPS Copyright and Licences
GPPS Licence Agreement
About the GPPS Journal
Aims and Scope
International Advisory Board
Editorial Board
Contact
Journal Home
Submissions
Editorial Processes
Submission and Manuscript Guidelines
Fees
Reviewer Guidelines
Permissions Guide for Authors
Indexing and Archiving
GPPS Editorial Policies
CrossMark, Correction and Retraction Policy
Journal issues
Terms & Conditions
Cookie Policy
Copyright Notice
Privacy Policy
GPPS Copyright and Licences
GPPS Licence Agreement
Author
Hisataka Fukushima
ORIGINAL ARTICLE
Unsteady flow mechanisms in the last stage of a transonic low pressure steam turbine - multistage effects and tip leakage flows
Ilias Papagiannis
,
Asad Raheem
,
Altug Basol
,
Anestis Kalfas
,
Reza Abhari
,
Hisataka Fukushima
,
Shigeki Senoo
J. Glob. Power Propuls. Soc. 2017;1:95–112
DOI
:
https://doi.org/10.22261/JGPPS.F4IW8S
Stats
Abstract
Article
(PDF)
Submit your paper
Journal issues
Most read
Month
Year
Improvement of corner separation prediction using an explicit non-linear RANS closure
Evaluation of ultra-high bypass ratio engines for an over-wing aircraft configuration
Influence of combined compressor and turbine deterioration on the overall performance of a jet engine using RANS simulation and Pseudo Bond Graph approach
Month
Year
Evaluation of ultra-high bypass ratio engines for an over-wing aircraft configuration
Influence of combined compressor and turbine deterioration on the overall performance of a jet engine using RANS simulation and Pseudo Bond Graph approach
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Indexes
Keywords index
Topics index
Authors index