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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
Author
Tim Williams
ORIGINAL ARTICLE
Low pressure ratio transonic fan stall with radial distortion
Tim S Williams
,
Cesare A Hall
,
Mark Wilson
J. Glob. Power Propuls. Soc. 2020;4:226–237
DOI
:
https://doi.org/10.33737/jgpps/130478
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Month
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Influence of combined compressor and turbine deterioration on the overall performance of a jet engine using RANS simulation and Pseudo Bond Graph approach
Evaluation of ultra-high bypass ratio engines for an over-wing aircraft configuration
Experimental evaluation of performance and mechanical reliability for high pressure CO2 integrally geared compressor
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
Loss Assessment of the Axial-Gap Size Effect in a Low-Pressure Turbine
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