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dc.contributor.authorWidnall, S. E.en_US
dc.contributor.authorBauer Paul E.en_US
dc.contributor.otherMassachusetts Institute of Technology. Flight Transportation Laboratoryen_US
dc.date.accessioned2012-01-06T22:01:44Z
dc.date.available2012-01-06T22:01:44Z
dc.date.issued1972en_US
dc.identifier13493240en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/68033
dc.descriptionAugust 1972en_US
dc.descriptionIncludes bibliographical references (leaf 12)en_US
dc.description.abstractAn open-jet wind tunnel operating within an anechoic chamber was developed for the purpose of the study of V/STOL noise mechanisms. An existing low-speed conventional hard-walled wind tunnel was modified to operate as an open-jet tunnel; an anechoic chamber was then constructed around the test section. The resulting aerodynamic and acoustic characteristics of the tunnel are discussed.en_US
dc.description.sponsorshipSponsored by ARO Durhamen_US
dc.format.extenti, 12 leavesen_US
dc.publisherCambridge, Mass. : Massachusetts Institute of Technology, Flight Transportation Laboratory, [1972]en_US
dc.relation.ispartofseriesFTL report (Massachusetts Institute of Technology. Flight Transportation Laboratory) ; R72-6en_US
dc.subjectWind tunnelsen_US
dc.subjectAerodynamic noiseen_US
dc.titleThe development of a wind tunnel facility for the study of V/STOL noiseen_US
dc.typeTechnical Reporten_US


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