Vortex generator effect on mitigation of separation in transonic flow nozzle

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dc.contributor.authorZare Shahneh, Amir
dc.date.accessioned2018-02-28T12:12:23Z
dc.date.available2018-02-28T12:12:23Z
dc.date.issued2015-04-30
dc.description.abstractThe effect of tetrahedral sub-boundary layer vortex generator on plummeting normal shock-induced turbulent boundary layer separation has been investigated in computational environment and the result is presented. A good agreement achieved in this work between the pre-assessed experimental and current CFD results, opens the way for further utilization of CFD in the area of shock/boundary layer interaction with 3-D mean compressible flow field, particularly for complicated geometries. The outcome style sheet is illustrated by the portions given in this document.en_UK
dc.identifier.citationA. Zare Shahneh. Vortex generator effect on mitigation of separation in transonic flow nozzle. International Journal of Advancements in Mechanical and Aeronautical Engineering, 2015, Volume 2, Issue 1, pp61-65en_UK
dc.identifier.issn2372-4153
dc.identifier.urihttps://www.seekdl.org/journals-details.py/98?years=2015&volumes=62&issue=142
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/13040
dc.language.isoenen_UK
dc.publisherInstitute of Research Engineers and Doctorsen_UK
dc.rightsCC0 1.0 Universal*
dc.rights.urihttp://creativecommons.org/publicdomain/zero/1.0/*
dc.subjectseparationen_UK
dc.subjectnormal shock waveen_UK
dc.subjectvortex generatoren_UK
dc.subjectCFDen_UK
dc.subjectSTAR-CDen_UK
dc.titleVortex generator effect on mitigation of separation in transonic flow nozzleen_UK
dc.typeArticleen_UK

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