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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
Keyword
shroud adaption
ORIGINAL ARTICLE
Influence of Different Gases on the Design Point of an Industrial Axial Compressor and Deduced Aerodynamical Rematching Methodology
Henrik Hoffmann
,
Lukas Stuhldreier
,
Ruben van Rennings
,
Peter Jeschke
J. Glob. Power Propuls. Soc. 2020;4:238–252
DOI
:
https://doi.org/10.33737/jgpps/130033
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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
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