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dc.contributor.authorT. Sato
dc.contributor.authorT. Nagayama
dc.contributor.authorS. Aoki
dc.date.accessioned2017-05-08T23:23:39Z
dc.date.available2017-05-08T23:23:39Z
dc.date.copyrightOctober, 1986
dc.date.issued1986
dc.identifier.issn0889-504X
dc.identifier.otherJOTUEI-28578#162_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/101822
dc.description.abstractRecently, a computer-aided interactive design system has been used for turbine design. The blade-to-blade flow program incorporated in the system is required to have short run times, robustness, and no limitations. The Denton time-marching code is attractive as it is fast and can handle mixed subsonic–supersonic flows. The Denton new scheme was published in 1982 and improvements were achieved in run times and entropy conservation. In this paper, code control variables are calibrated from the user’s point of view. Factors affecting computing costs and accuracy are investigated, and the “know-how” necessary to operate the code efficiently is discussed. Comparisons of calculated and experimental results are presented in part II.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleExtensive Verification of the Denton New Scheme From the User’s Point of View: Part I—Calibration of Code Control Variables
dc.typeJournal Paper
dc.journal.volume108
dc.journal.issue2
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.3262031
dc.journal.fristpage162
dc.journal.lastpage169
dc.identifier.eissn1528-8900
dc.treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 002
dc.contenttypeFulltext


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