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Jet flow field during screech

dc.contributor.authorSherman, P. M. (Pauline M.)en_US
dc.contributor.authorGlass, D. R. (D. Roger)en_US
dc.contributor.authorDuleep, K. G.en_US
dc.date.accessioned2006-09-08T19:39:00Z
dc.date.available2006-09-08T19:39:00Z
dc.date.issued1976-08en_US
dc.identifier.citationSherman, P. M.; Glass, D. R.; Duleep, K. G.; (1976). "Jet flow field during screech." Applied Scientific Research 32(3): 283-303. <http://hdl.handle.net/2027.42/41799>en_US
dc.identifier.issn0003-6994en_US
dc.identifier.issn1573-1987en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/41799
dc.description.abstractMeasurements were made of the flow field structure and the near field parameters of a jet exhausting from a sonic nozzle with a 1.27 cm exit diameter. Compressed air was used for obtaining stagnation pressures up to ∼5 atmospheres. The jet exhausted vertically from a settling chamber into an acoustically insulated room and through an insulated duct out through the roof. Measurements were made with several different reflecting surfaces at the nozzle exit as well as an insulating surface. Schlieren pictures at 500,000 frames/s were taken. Overall sound pressure level, impact pressure level downstream, and sound frequency analyzer measurements were made.en_US
dc.format.extent1547150 bytes
dc.format.extent3115 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.language.isoen_US
dc.publisherMartinus Nijhoff, The Hague/Kluwer Academic Publishers; Martinus Nijhoff ; Springer Science+Business Mediaen_US
dc.subject.otherPhysicsen_US
dc.subject.otherMechanicsen_US
dc.subject.otherAutomotive and Aerospace Engineeringen_US
dc.titleJet flow field during screechen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelScience insert into Categories values (General)en_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDept. of Aerospace Eng., The Univ. of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumDept. of Aerospace Eng., The Univ. of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumDept. of Aerospace Eng., The Univ. of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumcampusAnn Arboren_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/41799/1/10494_2004_Article_BF00411780.pdfen_US
dc.identifier.doihttp://dx.doi.org/10.1007/BF00411780en_US
dc.identifier.sourceApplied Scientific Researchen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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