Show simple item record

dc.contributor.authorJ. P. Smed
dc.contributor.authorN. Yamaguchi
dc.contributor.authorS. Umemura
dc.contributor.authorF. A. Pisz
dc.contributor.authorJ. A. Kain
dc.date.accessioned2017-05-08T23:39:54Z
dc.date.available2017-05-08T23:39:54Z
dc.date.copyrightApril, 1992
dc.date.issued1992
dc.identifier.issn0889-504X
dc.identifier.otherJOTUEI-28619#271_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/111086
dc.description.abstractAs part of the Westinghouse-MHI 501F development program, a new 16-stage axial flow compressor has been designed. Reported here are elements of the aerodynamic and mechanical design as well as general design features. Overall performance test results are also presented, which indicate that the compressor met or exceeded all expectations amenable to measurement during the full load shop test program.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.title501F Compressor Development Program
dc.typeJournal Paper
dc.journal.volume114
dc.journal.issue2
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.2929140
dc.journal.fristpage271
dc.journal.lastpage276
dc.identifier.eissn1528-8900
dc.keywordsCompressors
dc.keywordsStress
dc.keywordsDesign
dc.keywordsDesign engineering
dc.keywordsAxial flow AND Testing performance
dc.treeJournal of Turbomachinery:;1992:;volume( 114 ):;issue: 002
dc.contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record