Centrifugal Compressor Rate of Stability Assessment
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F25%3A00556014" target="_blank" >RIV/60162694:G43__/25:00556014 - isvavai.cz</a>
Result on the web
<a href="http://aimt.unob.cz/articles/20_01/1352.pdf" target="_blank" >http://aimt.unob.cz/articles/20_01/1352.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.3849/aimt.01352" target="_blank" >10.3849/aimt.01352</a>
Alternative languages
Result language
angličtina
Original language name
Centrifugal Compressor Rate of Stability Assessment
Original language description
Small jet and turboprop engines usually use centrifugal compressors. Compressor stable operation is very important for jet engine work and its use. This paper deals with centrifugal compressor stability margin assessment. The appropriate parameter is selected to inform us about working regime in which jet engine (compressor) works in terms of its stable operation.
Czech name
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Czech description
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Classification
Type
J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database
CEP classification
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OECD FORD branch
20301 - Mechanical engineering
Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2020
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
2533-4123
Volume of the periodical
15
Issue of the periodical within the volume
1
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
9
Pages from-to
115-123
UT code for WoS article
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EID of the result in the Scopus database
2-s2.0-85090730568