A method for computing the pressure distribution about an axisymmetric nacelle in subsonic flow

dc.contributor.author Trulin, Darryl
dc.contributor.department Aerospace Engineering
dc.date 2018-08-25T00:41:58.000
dc.date.accessioned 2020-07-02T05:43:36Z
dc.date.available 2020-07-02T05:43:36Z
dc.date.copyright Mon Jan 01 00:00:00 UTC 1968
dc.date.issued 1968
dc.format.mimetype application/pdf
dc.identifier archive/lib.dr.iastate.edu/rtd/4635/
dc.identifier.articleid 5634
dc.identifier.contextkey 6202680
dc.identifier.doi https://doi.org/10.31274/rtd-180813-3734
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath rtd/4635
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/77291
dc.language.iso en
dc.source.bitstream archive/lib.dr.iastate.edu/rtd/4635/r_6909898.pdf|||Sat Jan 15 00:23:24 UTC 2022
dc.subject.disciplines Aerospace Engineering
dc.subject.keywords Pressure
dc.subject.keywords Aerodynamics
dc.subject.keywords Airplanes--Nacelles
dc.subject.keywords Mechanical Engineering
dc.title A method for computing the pressure distribution about an axisymmetric nacelle in subsonic flow
dc.type article
dc.type.genre dissertation
dspace.entity.type Publication
relation.isOrgUnitOfPublication 047b23ca-7bd7-4194-b084-c4181d33d95d
thesis.degree.level dissertation
thesis.degree.name Doctor of Philosophy
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