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- W2370402374 abstract "In this paper,a two-dimensional numerical study on the stall of NACA 4415 airfoil is made by use of CFD.Pictures of the velocity contours,velocity vectors,and static pressure around the airfoil are given when it is submitted to five different attack angles and are compared with two-dimensional PIV experimental diagrams.As a good grip has been got on the stall characteristic of NACA4415 airfoil,the three-dimensional experiment on blades with tip vane can be carried out and the results can be predicted." @default.
- W2370402374 created "2016-06-24" @default.
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- W2370402374 date "2009-01-01" @default.
- W2370402374 modified "2023-09-23" @default.
- W2370402374 title "A TWO-DIMENSIONAL NUMERICAL STUDY ON STALL OF NACA4415 AIRFOIL" @default.
- W2370402374 hasPublicationYear "2009" @default.
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