A Theoretical Basis for the Scaling Law of Broadband Shock Noise Intensity in Supersonic Jets

<table>Comparison of the present theory and the data of Tanna [<a href="/journals/aav/2011/573209/#B22">22</a>] for the intensity of the broadband shock noise.</table>

Advances in Acoustics and Vibration

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Figure 9

Figure 9: A Theoretical Basis for the Scaling Law of Broadband Shock Noise Intensity in Supersonic Jets 