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dc.contributor.authorSabnis, Kshitij
dc.contributor.authorBoscagli, Luca
dc.contributor.authorSwarthout, Avery
dc.contributor.authorBabinsky, Holger
dc.contributor.authorMacManus, David
dc.contributor.authorSheaf, Christopher
dc.date.accessioned2022-04-22T23:30:21Z
dc.date.available2022-04-22T23:30:21Z
dc.date.issued2022-03-28
dc.identifier.urihttps://www.repository.cam.ac.uk/handle/1810/336382
dc.description.abstractUltra high-bypass ratio engines, which show considerable promise in reducing the environmental impact of commercial aviation, generally adopt slim fan cowl profiles. These geometries can be more sensitive to separation on the external surfaces in engine windmilling con- ditions during take-off climb out or during cruise. This paper describes the development of a two-dimensional wind tunnel rig which can accurately replicate the separation mechanisms experienced by real aero-engine nacelles. This design process highlights the importance of considering factors such as Reynolds-number effects, tunnel-wall effects, the two-dimensional nature of the rig, and the tunnel boundary layers.
dc.description.sponsorshipThis project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement No 101007598. The JU receives support from the European Union’s Horizon 2020 research and innovation programme and the Clean Sky 2 JU members other than the Union.
dc.rightsAll Rights Reserved
dc.rights.urihttp://www.rioxx.net/licenses/all-rights-reserved
dc.titleDesign of a New Test Rig to Investigate Transonic External Fan Cowl Separation
dc.typeConference Object
dc.publisher.departmentDepartment of Engineering
dc.date.updated2022-04-22T07:58:30Z
prism.publicationDate2022
dc.identifier.doi10.17863/CAM.83799
dcterms.dateAccepted2021-12-14
rioxxterms.versionofrecord10.17863/CAM.83799
rioxxterms.versionAM
dc.contributor.orcidSabnis, Kshitij [0000-0001-7609-2923]
pubs.funder-project-idEuropean Commission Horizon 2020 (H2020) Industrial Leadership (IL) (101007598)
cam.issuedOnline2022-03-28
pubs.conference-name56th 3AF International Conference on Applied Aerodynamics
pubs.conference-start-date2022-03-28
cam.orpheus.successMon Apr 25 18:24:19 BST 2022 - Embargo updated
cam.depositDate2022-04-22
pubs.conference-finish-date2022-03-30
pubs.licence-identifierapollo-deposit-licence-2-1
pubs.licence-display-nameApollo Repository Deposit Licence Agreement
rioxxterms.freetoread.startdate2023-03-28


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