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Shock and Vibration
/
2021
/
Article
/
Tab 1
/
Research Article
Transition Effect on the Flow Dynamics in a Compressor Blade Passage
Table 1
Step location on the compressor blade.
Strip location (-)
X
/
C
= 0.02
X
/
C
= 0.16
Strip width (mm)
5
5
Step height (
μ
m)
100
100