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Shock and Vibration
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Shock and Vibration
/
2021
/
Article
/
Tab 2
/
Research Article
Transition Effect on the Flow Dynamics in a Compressor Blade Passage
Table 2
Roughness strip location and its average height (Ra) on the compressor blade.
Strip location (-)
X
/
C
= 0.11
X
/
C
= 0.16
X
/
C
= 0.21
Strip width (mm)
10
5
5
Roughness height Ra (
μ
m)
8
12
12
10
16
16
12
20
20