{"@context":{"@vocab":"https://cir.nii.ac.jp/schema/1.0/","rdfs":"http://www.w3.org/2000/01/rdf-schema#","dc":"http://purl.org/dc/elements/1.1/","dcterms":"http://purl.org/dc/terms/","foaf":"http://xmlns.com/foaf/0.1/","prism":"http://prismstandard.org/namespaces/basic/2.0/","cinii":"http://ci.nii.ac.jp/ns/1.0/","datacite":"https://schema.datacite.org/meta/kernel-4/","ndl":"http://ndl.go.jp/dcndl/terms/","jpcoar":"https://github.com/JPCOAR/schema/blob/master/2.0/"},"@id":"https://cir.nii.ac.jp/crid/1363670320744997120.json","@type":"Article","productIdentifier":[{"identifier":{"@type":"DOI","@value":"10.1115/1.3446138"}},{"identifier":{"@type":"URI","@value":"http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/98/2/190/5886245/190_1.pdf"}}],"dc:title":[{"@value":"Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model"}],"description":[{"type":"abstract","notation":[{"@value":"<jats:p>This paper reports a theoretical study of axial compressor surge. A nonlinear model is developed to predict the transient response of a compression system subsequent to a perturbation from steady operating conditions. It is found that for the system investigated there is an important nondimensional parameter on which this response depends. Whether this parameter is above or below a critical value determines which mode of compressor instability, rotating stall or surge, will be encountered at the stall line. For values above the critical, the system will exhibit the large amplitude oscillatory behavior characteristic of surge; while for values below the critical it will move toward operation in rotating stall, at a substantially reduced flow rate and pressure ratio. Numerical results are presented to show the motion of the compression system operating point during these two basic modes of instability, and a physical explanation is given for the mechanism associated with the generation of surge cycle oscillations.</jats:p>"}]}],"creator":[{"@id":"https://cir.nii.ac.jp/crid/1380285706452508290","@type":"Researcher","foaf:name":[{"@value":"E. M. Greitzer"}],"jpcoar:affiliationName":[{"@value":"Compressor Group, Pratt & Whitney Aircraft, East Hartford, Ct."}]}],"publication":{"publicationIdentifier":[{"@type":"PISSN","@value":"00220825"}],"prism:publicationName":[{"@value":"Journal of Engineering for Power"}],"dc:publisher":[{"@value":"ASME International"}],"prism:publicationDate":"1976-04-01","prism:volume":"98","prism:number":"2","prism:startingPage":"190","prism:endingPage":"198"},"reviewed":"false","url":[{"@id":"http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/98/2/190/5886245/190_1.pdf"}],"createdAt":"2010-11-03","modifiedAt":"2019-11-07","relatedProduct":[{"@id":"https://cir.nii.ac.jp/crid/1360025430208377984","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@value":"Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor"}]},{"@id":"https://cir.nii.ac.jp/crid/1360285706452508160","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@value":"Coexisting state of surge and rotating stall in a two-stage axial flow compressor using a double-phase-locked averaging technique"}]},{"@id":"https://cir.nii.ac.jp/crid/1360298336549001984","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@value":"Effect of pulsating flow on mild / deep surge phenomena of turbocharger compressor"}]},{"@id":"https://cir.nii.ac.jp/crid/1360576118753173760","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@value":"Effect of Pulsating Flow on Surge Frequency of a Turbocharger Compressor"}]},{"@id":"https://cir.nii.ac.jp/crid/1390001205296999424","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"A Study on the Fundamental Surge Frequencies in Multi-Stage Axial Flow Compressor Systems"}]},{"@id":"https://cir.nii.ac.jp/crid/1390001205298563968","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Genesis of Researches on Surges in Pumping Systems in Japan"}]},{"@id":"https://cir.nii.ac.jp/crid/1390282680222871552","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Experimental investigation on unstable flow in multi-stage centrifugal blower with inlet guide vane"}]},{"@id":"https://cir.nii.ac.jp/crid/1390282680275115264","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Analytical Study on Stall Stagnation Boundaries in Axial-Flow Compressor and Duct Systems"}]},{"@id":"https://cir.nii.ac.jp/crid/1390282680275135616","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Development of a Simulation Method of Surge Transient Flow Phenomena in a Multistage Axial Flow Compressor and Duct System"}]},{"@id":"https://cir.nii.ac.jp/crid/1390282680275269888","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Analytical Surge Behaviors in Systems of a Single-stage Axial Flow Compressor and Flow-paths"}]},{"@id":"https://cir.nii.ac.jp/crid/1390867611167624704","@type":"Article","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@language":"en","@value":"Experimental and numerical analyses of mild surge in a transonic centrifugal compressor with a vaneless diffuser"}]}],"dataSourceIdentifier":[{"@type":"CROSSREF","@value":"10.1115/1.3446138"},{"@type":"CROSSREF","@value":"10.5293/ijfms.2016.9.1.001_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1299/jfst.2016jfst0009_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1115/1.4066814_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1007/s11630-017-0907-x_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.5293/ijfms.2013.6.2.056_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1088/1742-6596/2217/1/012083_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.5293/ijfms.2016.9.1.017_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1088/1742-6596/1909/1/012084_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.1299/jfst.2025jfst0011_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.5293/ijfms.2013.6.4.189_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"},{"@type":"CROSSREF","@value":"10.5293/ijfms.2014.7.4.160_references_DOI_8UiHeRlOaHInjIYH18AlatgOKuw"}]}