Mode Switching in a Compressible Rectangular Cavity Flow

Author:

Huang Yi-Xuan1,Chung Kung-Ming2ORCID

Affiliation:

1. Department of Aeronautics and Astronautics, National Cheng Kung University, Tainan 701, Taiwan

2. Aerospace Science and Technology Research Center, National Cheng Kung University, Tainan 711, Taiwan

Abstract

This study determines the mean and fluctuating pressures for flow through a rectangular shallow cavity (ratio between the length and the depth = 2.43, 4.43, and 6.14; ratio between the length and the width = 0.5, 1.0, and 2.0) at a Mach number of 0.64 in a blowdown transonic wind tunnel. A amplitude modulation analysis is used for the post-processing of the fluctuating pressure signals. The spectral analysis (wavelet) shows the intermittent behavior of the discrete Rossiter–Heller modes. A correlation analysis determines that mode switching is more significant between the second and third modes (organized structures that are associated with shear layer vortices), particularly for two-dimensional and shallower cavities.

Funder

National Science and Technology Council Taiwan

Publisher

MDPI AG

Subject

Aerospace Engineering

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