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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2016
/
Article
/
Tab 1
Research Article
Effects of Freestream Turbulence on Cavity Tone and Sound Source
Table 1
Computational and experimental conditions.
Tu
θ
/
L
Computation
0.5
0.0
—
0.0071
0.09
0.9
0.095
0.0072
1.5
0.078
0.0074
1.8
0.090
0.0077
2.3
0.111
0.0078
Computation
2.5
0.0
—
0.0071
0.09
0.9
0.095
0.0072
1.5
0.078
0.0074
1.8
0.090
0.0077
2.3
0.111
0.0078
Experiment
0.5
0.6
0.165
0.0072
0.09
2.5