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dc.contributor.authorMATSUSHITA, Michinorien
dc.contributor.authorAKAMATSU, Teruakien
dc.date.accessioned2023-03-28T09:07:02Z-
dc.date.available2023-03-28T09:07:02Z-
dc.date.issued1977-03-31-
dc.identifier.urihttp://hdl.handle.net/2433/281023-
dc.description.abstractA numerical analysis was made for a dissociative reflected shock wave and its invicid flow field, and for unsteady thermal and concentration boundary layers developing at the end wall of a shock tube. It was shown that an entropy layer is formed adjacent to the end wall. The thermal boundary layer was found to have an overshoot of temperature which was sometimes higher than that outside the boundary layer. The concentration boundary layer was found to develop mainly due to the convection of highly dissociated gases from outside the boundary layer. It was found that self-similar boundary layers become valid finally.en
dc.language.isoeng-
dc.publisherFaculty of Engineering, Kyoto Universityen
dc.publisher.alternative京都大学工学部ja
dc.subject.ndc500-
dc.titleEffects of Dissociation Relaxation upon Reflected Shock Waves and Unsteady Thermal Boundary Layersen
dc.typedepartmental bulletin paper-
dc.type.niitypeDepartmental Bulletin Paper-
dc.identifier.ncidAA00732503-
dc.identifier.jtitleMemoirs of the Faculty of Engineering, Kyoto Universityen
dc.identifier.volume39-
dc.identifier.issue1-
dc.identifier.spage103-
dc.identifier.epage121-
dc.textversionpublisher-
dc.sortkey08-
dc.addressDepartment of Mechanical Engineeringen
dc.addressDepartment of Mechanical Engineeringen
dcterms.accessRightsopen access-
dc.identifier.pissn0023-6063-
出現コレクション:Vol.39 Part 1

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