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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.06.045
Abstract: Abstract Modern turbomachinery design uses the endwall treatment method to prevent the corner flow from separating. This study presents the Blended Blade and End Wall (BBEW) method, a passive endwall treatment method, and draws the…
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Keywords:
blade end;
method;
blended blade;
pressure difference ... See more keywords
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Published in 2021 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2021.107032
Abstract: Abstract The strong adverse pressure gradient and shock wave/boundary layer interaction that occurs in supersonic compressor cascade corner regions usually leads to large three-dimensional corner separations with extensive total pressure losses. This substantially restricts compressor…
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Keywords:
end slot;
blade end;
corner separation;
corner ... See more keywords
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2
Published in 2022 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100221138163
Abstract: Blended Blade and End Wall (BBEW), a passive control method, has been employed in the turbomachinery field and verified to improve compressor performance effectively. In this paper, a new profiling method, based on suction surface…
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Keywords:
blended blade;
control;
design;
three dimensional ... See more keywords
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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j058488
Abstract: The proposed passive control method, blade-end slots, is implemented to reorganize the blade-end flow in a highly loaded compressor cascade under a wide incidence range at Ma=0.59. Both experimenta...
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Keywords:
highly loaded;
control;
loaded compressor;
end slots ... See more keywords