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Influence of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors
Hao FU,
Ling ZHOU
*
, Lucheng JI
*
Corresponding author for this work
School of Aerospace Engineering
Beijing Institute of Technology
Tsinghua University
Research output
:
Contribution to journal
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Article
›
peer-review
11
Citations (Scopus)
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Dive into the research topics of 'Influence of sub boundary layer vortex generator height and attack angle on cross-flows in the hub region of compressors'. Together they form a unique fingerprint.
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Engineering
Boundary Layer
100%
Attack Angle
100%
Vortex Generator
100%
Vortex
50%
Angle-of-Attack
25%
Flat Plate
25%
Flow Phenomenon
25%
Controlling Mechanism
25%
Additional Loss
25%