Velocity Field Calculation and Measurement at the Inlet of Centrifugal Compressor
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F09%3A%230002807" target="_blank" >RIV/60162694:G43__/09:#0002807 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Velocity Field Calculation and Measurement at the Inlet of Centrifugal Compressor
Original language description
This paper is focused on 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 of the slots, through which the external airenters the main air in the intake system, the flow velocities at the impeller inlet were measured and calculated.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JT - Propulsion, engines and fuels
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2009
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
ADVANCES IN MILITARY TECHNOLOGY
ISSN
1802-2308
e-ISSN
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Volume of the periodical
4
Issue of the periodical within the volume
2
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
12
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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