Measurement of Coherent Flow Instabilities in The Wake of a Compressor Blade at High Incidence Angles
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F24%3A00602720" target="_blank" >RIV/61388998:_____/24:00602720 - isvavai.cz</a>
Result on the web
<a href="https://www.meastechturbo.com/paper-archives/mtt2723-larnaca-2024-abstracts/item/623-measurement-of-coherent-flow-instabilities-in-the-wake-of-a-compressor-blade-at-high-incidence-angles" target="_blank" >https://www.meastechturbo.com/paper-archives/mtt2723-larnaca-2024-abstracts/item/623-measurement-of-coherent-flow-instabilities-in-the-wake-of-a-compressor-blade-at-high-incidence-angles</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Measurement of Coherent Flow Instabilities in The Wake of a Compressor Blade at High Incidence Angles
Original language description
The study reports on preliminary measurements of coherent instabilities in the separated flow downstream of blade with a transonic compressor profile, registered by Kulite dynamic pressure transducers mounted in the blade surface. For the sake of future investigation of non-synchronous vibration, the frequency and amplitude of the spectral peak was analyzed for various blade incidence angles and inlet Mach numbers.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
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OECD FORD branch
20302 - Applied mechanics
Result continuities
Project
<a href="/en/project/LUAUS23231" target="_blank" >LUAUS23231: Origins and mechanisms of flutter and non-synchronous vibration in modern turbomachines operating at wide range of regimes</a><br>
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2024
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů