Abstract
A supersonic flow over a rectangular cavity is known to oscillate at certain predominant frequencies. The present study focuses on the effect of the cavity length-to-depth (L/D) ratio on the frequency for a free-stream Mach number of 1.7. The pressure oscillations are measured by changing the L/D ratio from 0.5 to 3.0, and the power spectral density is calculated from the temporal pressure signals for each L/D ratio. The results demonstrate that the spectral peaks for an L/D ratio of less than 1 and greater than 2 are accounted for by the feedback mechanisms of the transverse and longitudinal oscillations, respectively. The results also demonstrate that the spectral peaks in the transition (1
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CITATION STYLE
Handa, T., Tanigawa, K., Kihara, Y., Miyachi, H., & Kakuno, H. (2015). Frequencies of Transverse and Longitudinal Oscillations in Supersonic Cavity Flows. International Journal of Aerospace Engineering, 2015. https://doi.org/10.1155/2015/751029
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