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Shock and Vibration
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Shock and Vibration
/
2019
/
Article
/
Tab 1
/
Research Article
Numerical Simulation Study on Aeroacoustic Characteristics within Deformable Cavities
Table 1
Positions of monitoring points.
Ceiling
Monitor
x
/
L
1
K
20
0.05
2
K
21
0.15
3
K
22
0.25
4
K
23
0.35
5
K
24
0.45
6
K
25
0.55
7
K
26
0.65
8
K
27
0.75
9
K
28
0.85
10
K
29
0.95