Influence of Active Methods of Flow Control on Compressor Blade Cascade Flow

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F08%3A00144768" target="_blank" >RIV/68407700:21220/08:00144768 - 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
Influence of Active Methods of Flow Control on Compressor Blade Cascade Flow
Original language description
This paper deals with active methods of flow control, especially synthetic jet flow control. A synthetic jet was used for flow control in the compressor blade cascade to reduce the vortex structure and reduce the value of the loss coefficients. The output slot of the synthetic jet actuator was situated on the side wall on the connecting line of the leading edges of the blades. The direction of the synthetic jet was perpendicular to the main flow. The synthetic jet excitation is more effective and more efficient than a steady blowing or suction, and its great advantage is zero mass flux supplied to, or taken from the main flow. A positive influence of the synthetic jet on the flow field was proved. The flow field was also visualized.
Czech name
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Czech description
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Project
<a href="/en/project/1M06059" target="_blank" >1M06059: Advanced Technologies and Systems for Power Engineering</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2008
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ASME Turbo Expo 2008, Power for Land, Sea and Air
ISBN
978-0-7918-4316-1
ISSN
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e-ISSN
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Number of pages
9
Pages from-to
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Publisher name
American Society Of Mechanical Engineers - ASME
Place of publication
New York
Event location
Berlin
Event date
Jun 9, 2008
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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