Show simple item record

dc.contributor.authorMohankumar, Benjamin
dc.date.accessioned2022-01-25T02:52:36Z
dc.date.available2022-01-25T02:52:36Z
dc.date.submitted2021-04-30
dc.identifier.urihttps://www.repository.cam.ac.uk/handle/1810/332907
dc.description.abstract[Restricted]
dc.description.sponsorshipRolls-Royce plc.
dc.rightsAll Rights Reserved
dc.rights.urihttps://www.rioxx.net/licenses/all-rights-reserved/
dc.subjectaerodynamics
dc.subjectturbomachinery
dc.subjectgas turbine
dc.subjectaerospace
dc.subjectaviation
dc.subjectengineering
dc.subjectdesign
dc.titleTransonic Fan Design for a Separated Intake at High Angle of Attack
dc.typeThesis
dc.type.qualificationlevelDoctoral
dc.type.qualificationnameDoctor of Philosophy (PhD)
dc.publisher.institutionUniversity of Cambridge
dc.date.updated2022-01-23T16:41:11Z
dc.identifier.doi10.17863/CAM.80337
rioxxterms.licenseref.urihttps://www.rioxx.net/licenses/all-rights-reserved/
rioxxterms.typeThesis
dc.publisher.collegeSt Johns
pubs.funder-project-idTechnology Strategy Board (113075)
cam.supervisorHall, Cesare
cam.depositDate2022-01-23
pubs.licence-identifierapollo-deposit-licence-2-1
pubs.licence-display-nameApollo Repository Deposit Licence Agreement


Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record