A Robust Mixing Plane and Its Application in Three-Dimensional Inverse Design of Transonic Turbine Stages
- Submitting institution
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University College London
- Unit of assessment
- 12 - Engineering
- Output identifier
- 11926
- Type
- D - Journal article
- DOI
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10.1115/1.4028216
- Title of journal
- JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
- Article number
- ARTN 011004
- First page
- -
- Volume
- 137
- Issue
- 1
- ISSN
- 0889-504X
- Open access status
- Out of scope for open access requirements
- Month of publication
- September
- Year of publication
- 2014
- URL
-
-
- Supplementary information
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-
- 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
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1
- Research group(s)
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-
- Proposed double-weighted
- No
- Reserve for an output with double weighting
- No
- Additional information
- The paper presents the development of a novel mixing plane model for application to 3D inverse design of multistage transonic turbomachines. The 3D inverse design method can be used for direct control and reduction of shockwave strength in transonic axial compressors with significant improvement in efficiency of aeroengines and gas turbine. The methodology is now being developed into a commercial software by Advanced Design Technology Ltd ( adtechnology.com - a spin out company from UCL) and currently is being considered by Safran, a major Franch Aeroengine manufacturer ( contact: Francois JULIENNE, Team Leader Methods, Email: francois.julienne@safrangroup.com).
- Author contribution statement
- -
- Non-English
- No
- English abstract
- -