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Integrated design of compressor transition ducts with swirling flow and aerodynamic lifting struts
Integrated design of compressor transition ducts with swirling flow and aerodynamic lifting struts
Funding
European Union Seventh Framework Program under grant agreement n° 283216, LEMCOTEC (Low Emission Core Engine Technologies)
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Publisher
Loughborough UniversityRights holder
© I.L. MariahPublication date
2018Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of the degree of Doctor of Philosophy at Loughborough University.Language
- en
Supervisor(s)
A.D. Walker ; J.F. CarrotteQualification name
- PhD
Qualification level
- Doctoral
This submission includes a signed certificate in addition to the thesis file(s)
- I have submitted a signed certificate
