Experimental Identification of a New Secondary Wave Pattern in Transonic Cascades with Porous Walls
Experimental Identification of a New Secondary Wave Pattern in Transonic Cascades with Porous Walls
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Basel: MDPI AG
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Language
English
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Basel: MDPI AG
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Contents
Turbomachinery shock wave patterns occur as a natural result of operating at off-design points and are accountable for some of the loss in performance. In some cases, shock wave–boundary layer (SW-BLIs) interactions may even lead to map restrictions. The current paper refers to experimental findings on a transonic linear cascade specifically design...
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Experimental Identification of a New Secondary Wave Pattern in Transonic Cascades with Porous Walls
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TN_cdi_doaj_primary_oai_doaj_org_article_6325c56e3b054f089e264510da28f96f
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_6325c56e3b054f089e264510da28f96f
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ISSN
2226-4310
E-ISSN
2226-4310
DOI
10.3390/aerospace11110946
