Ice crystal icing in gas turbine engines - ORA - Oxford University Research Archive

Abstract:: High altitude ice particles can accrete inside the core compression system of turbofan engines in cruise and descent. This can lead to severe in-flight events including blade damage, surge and flameout. This thesis describes the development and validation of a new comprehensive computational model to aid prediction of ice crystal icing in turbofan compressors. The Ice Crystal Icing ComputationaL Environment (ICICLE) delivers a step change in modelling of the phenomenon compared to the ...
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APA Style

Bucknell, A. (2018). Ice crystal icing in gas turbine engines [PhD thesis]. University of Oxford.

MLA Style

Bucknell, A. Ice Crystal Icing in Gas Turbine Engines. 2018. University of Oxford, PhD thesis.

Chicago Style

Bucknell, A. 2018. “Ice Crystal Icing in Gas Turbine Engines.” PhD thesis, University of Oxford.
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Files:: Bucknell_2018_Ice_crystal_icing.pdf

(Preview, Dissemination version, pdf, 15.2MB, Terms of use)

Authors

+ Bucknell, A More by this author

Division:: MPLS
Department:: Engineering Science
Role:: Author

Contributors

Role:: Supervisor

Role:: Supervisor

+ Engineering and Physical Sciences Research Council More from this funder

Grant:: EP/L015943/1

+ Rolls-Royce Plc More from this funder

Type of award:: DPhil
Level of award:: Doctoral
Awarding institution:: University of Oxford

UUID:: uuid:d7b0dace-d5a1-490f-9e1c-02ff42d4d649
Deposit date:: 2019-05-08
ARK identifier:: ark:/29072/ora_d7b0daced5a1490f9e1c02ff42d4d649

Terms of use

Copyright holder:: Bucknell, A
Copyright date:: 2018

Licence:: Terms and Conditions of Use for Oxford University Research Archive

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