Asymptotic solution of transonic nozzle flows with homogeneous condensation. II. Supercritical flows

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dc.citation.epage2995en_US
dc.citation.issueNumber11en_US
dc.citation.spage2982en_US
dc.citation.volumeNumber5en_US
dc.contributor.authorDelale, C. F.en_US
dc.contributor.authorSchnerr, G. H.en_US
dc.contributor.authorZierep, J.en_US
dc.date.accessioned2016-02-08T10:54:55Z
dc.date.available2016-02-08T10:54:55Z
dc.date.issued1992en_US
dc.departmentDepartment of Mathematicsen_US
dc.description.abstractA detailed analysis of supercritical transonic nozzle flows with stationary normal shock waves is presented. A classification scheme based on the normal shock location is obtained using asymptotic methods, and four distinct supercritical flow regimes are distinguished. A simple shock fitting technique that determines the shock location within any desired precision is introduced. Consequently, an algorithm that exhibits the asymptotic solution in each supercritical flow regime is developed for the expansion of moist air in nozzles with atmospheric supply conditions by utilizing the classical nucleation theory and the Hertz-Knudsen droplet growth law. Good agreement with the recent static pressure measurements and visualized shock locations is achieved in relatively slender nozzles when the condensed phase is assumed to consist purely of water drops. © 1993 American Institute of Physics.en_US
dc.identifier.doi10.1063/1.858705en_US
dc.identifier.eissn2163-5013
dc.identifier.issn0899-8213
dc.identifier.urihttp://hdl.handle.net/11693/26093
dc.language.isoEnglishen_US
dc.publisherA I P Publishing LLCen_US
dc.relation.isversionofhttps://doi.org/10.1063/1.858705en_US
dc.source.titlePhysics of Fluids Aen_US
dc.titleAsymptotic solution of transonic nozzle flows with homogeneous condensation. II. Supercritical flowsen_US
dc.typeArticleen_US
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