Velocity field measurements at the inlet of centrifugal compressor

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F08%3A%230002808" target="_blank" >RIV/60162694:G43__/08:#0002808 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Velocity field measurements at the inlet of centrifugal compressor

Original language description

This paper describes the possibilities of extending the stable operation region of the centrifugal air compressor by modifying its intake system. For various compressor operation regimes and various shapes and directions of the slots, through which the external air flow enters the main air flow intake system, the flow velocities, at the impeller inlet were measured.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JT - Propulsion, engines and fuels

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2008

Confidentiality

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

Name of the periodical

Acta Avionica

ISSN

1335-9479

e-ISSN

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Volume of the periodical

10

Issue of the periodical within the volume

16

Country of publishing house

SK - SLOVAKIA

Number of pages

6

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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