Optimization Design of Compressor Cascade with Swept and Curved Blades
43rd:; meeting.; MEETING AND EXHIBIT, Aerospace sciences ; 2005 ; Reno, NV
01.01.2005
AIAA 2005-336
2005-0019 - 2005-1421 with gaps
Aufsatz (Konferenz)
Englisch
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Stall Margin Enhancement of Aeroengine Compressor with a Novel Type of Alternately Swept Blades
British Library Conference Proceedings | 2020
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