Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F26%3A0199104" target="_blank" >RIV/00216305:26210/26:0199104 - isvavai.cz</a>

Result on the web

<a href="https://asmedigitalcollection.asme.org/turbomachinery/article/148/1/011007/1220989/Aerodynamic-Effect-of-Shallow-Circumferential" target="_blank" >https://asmedigitalcollection.asme.org/turbomachinery/article/148/1/011007/1220989/Aerodynamic-Effect-of-Shallow-Circumferential</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1115/1.4069422" target="_blank" >10.1115/1.4069422</a>

Result language

angličtina

Original language name

Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor

Original language description

The standard aerodynamic design of a centrifugal compressor features an unshrouded impeller with a smooth shroud. However, the shape of the shroud significantly influences the final compressor parameters. Previous research has shown that even small geometric changes in the shroud, referred to as casing treatment, can substantially affect the operating characteristics of a rotating machine. This article presents a novel casing treatment for a centrifugal compressor, involving the creation of ten circumferential grooves with a semi-circular profile in a meridional section. The radius of these grooves is approximately equal to the tip clearance. Experimental results demonstrate that the presence of these grooves shifts the surge line toward lower flowrates, increases efficiency in a narrow region between the best efficiency point and the surge line and shifts the choke line toward lower flowrates. External sound pressure measurements indicate a reduction in amplitudes at sub-synchronous frequencies, suggesting a potential link between the compressor map's influence and the suppression of aerodynamic instabilities. Computational fluid dynamics analysis supports the experimental observations, revealing a significant influence of energy dissipation caused by the applied grooves. This study highlights the considerable impact of shroud geometry on centrifugal compressors with unshrouded impellers and offers valuable insights for further research into casing treatments.

Czech name

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Czech description

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Type

J_imp - Article in a specialist periodical, which is included in the Web of Science database

CEP classification

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OECD FORD branch

20300 - Mechanical engineering

Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2026

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Journal of Turbomachinery

ISSN

0889-504X

e-ISSN

1528-8900

Volume of the periodical

1

Issue of the periodical within the volume

148

Country of publishing house

US - UNITED STATES

Number of pages

11

Pages from-to

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UT code for WoS article

001629683700008

EID of the result in the Scopus database

2-s2.0-105015643065