Frequencies of Transverse and Longitudinal Oscillations in Supersonic Cavity Flows. (20th October 2015)

• Record Type: Journal Article
• Authors: Handa, Taro; Tanigawa, Kazuya; Kihara, Yusuke; Miyachi, Hiroaki; Kakuno, Hatsuki
• Other Names: Chang Keh-Chin Academic Editor.
• Is Part Of: International journal of aerospace engineering. Volume 2015(2015)
• Publication Date: 2015-10-20
• Subjects: Aerospace engineering -- Periodicals; 629.105
• DOI: 10.1155/2015/751029
• Languages: English
• ISSNs: 1687-5966

Abstract

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 theL / D ratio from 0.5 to 3.0, and the power spectral density is calculated from the temporal pressure signals for eachL / D ratio. The results demonstrate that the spectral peaks for anL / 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 <~L / D <~ 2) are accounted for by either of the two feedback mechanisms of transverse and longitudinal oscillations; that is, the flows under the transition regime oscillate both transversely and longitudinally.