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contributor authorKarl E. Wichert
date accessioned2017-05-09T01:08:02Z
date available2017-05-09T01:08:02Z
date copyrightJuly, 1961
date issued1961
identifier issn1528-8919
identifier otherJETPEZ-26617#286_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154834
description abstractA design for a transonic axial-flow compressor is described, in which a rotor wheel with a low degree of reaction operates in subsonic flow and the stator operates in supersonic flow. A compressor was run as a single-stage compressor and an outlet pressure ratio equal to that of an orthodox compressor with 4 stages. Some discussion of another compressor in which both the rotor wheel and the stator operate in supersonic flow is also given.
publisherThe American Society of Mechanical Engineers (ASME)
titleSome Investigations Into Transonic Axial-Flow Compressors With High Stage Load Coefficients and Low Degrees of Reaction
typeJournal Paper
journal volume83
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3673189
journal fristpage286
journal lastpage290
identifier eissn0742-4795
keywordsCompressors
keywordsStress
keywordsAxial flow
keywordsStators
keywordsSupersonic flow
keywordsWheels
keywordsRotors
keywordsPressure
keywordsDesign AND Subsonic flow
treeJournal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 003
contenttypeFulltext


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