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contributor authorH. Hayami
contributor authorY. Senoo
contributor authorK. Utsunomiya
date accessioned2017-05-08T23:34:09Z
date available2017-05-08T23:34:09Z
date copyrightJanuary, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28600#25_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107780
description abstractLow-solidity circular cascades, conformally transformed from high-stagger linear cascades of double-circular-arc vanes with solidity 0.69, were used as a part of the diffuser system of a transonic centrifugal compressor. Performance test results were compared with data of the same compressor with a vaneless diffuser. Good compressor performance and a wider flow range as well as a higher pressure ratio and a higher efficiency, superior to those with a vaneless diffuser, where the flow range was limited by choke of the impeller, were demonstrated. The test circular cascade diffusers demonstrated a good pressure recovery over a wide range of flow angles, even when the inflow Mach number to the cascade was over unity.
publisherThe American Society of Mechanical Engineers (ASME)
titleApplication of a Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor
typeJournal Paper
journal volume112
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927416
journal fristpage25
journal lastpage29
identifier eissn1528-8900
keywordsCompressors
keywordsCascades (Fluid dynamics)
keywordsDiffusers
keywordsFlow (Dynamics)
keywordsVaneless diffusers
keywordsPressure
keywordsInflow
keywordsTesting performance
keywordsMach number AND Impellers
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 001
contenttypeFulltext


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