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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