Areal parametric characterisation of ex-service compressor blade leading edges
- Submitting institution
-
The University of Huddersfield
- Unit of assessment
- 12 - Engineering
- Output identifier
- 40
- Type
- D - Journal article
- DOI
-
10.1016/j.wear.2014.10.007
- Title of journal
- Wear
- Article number
- -
- First page
- 79
- Volume
- 321
- Issue
- -
- ISSN
- 0043-1648
- Open access status
- Out of scope for open access requirements
- Month of publication
- October
- Year of publication
- 2014
- URL
-
-
- Supplementary information
-
-
- Request cross-referral to
- -
- Output has been delayed by COVID-19
- No
- COVID-19 affected output statement
- -
- Forensic science
- No
- Criminology
- No
- Interdisciplinary
- No
- Number of additional authors
-
4
- Research group(s)
-
-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- This publication forms part of a PhD and wider ongoing project with Rolls-Royce plc and Cambridge University. The research involved the development of techniques to characterise and correlate gas washed surface finish with drag loss. The value of the project to Rolls-Royce has been demonstrated with directly related and ongoing research across a number of departments including: Turbine statics, Turbines Aerothermal, Compressors, and Civil aerospace experimental and in collaboration with Rolls-Royce engineers including: Frederic.Goenaga@Rolls-Royce.com, David.Newman@Rolls-Royce.com, Dougal.Jackson@Rolls-Royce.com, David.Lambie@Rolls-Royce.com, Michael.Whittle@Rolls-Royce.com. Currently, negotiations to develop deeper knowledge transfer into Rolls by way of KTP are under way.
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -
