Abstract
Flow over an isolated shallow open-type rectangular cavity was investigated experimentally. Pressure measurements at Mach numbers 0.3, 0.5 and 0.6 were performed. Turbulent boundary layer was naturally developed along a flat plate upstream the cavity. During the experiments two test configurations were employed. Strong resonance was observed in the pressure signals obtained at M = 0.5 and M = 0.6 for the test configuration with the short upstream plate. Instantaneous oscillating characteristics were studied by Wavelet and Hilbert-Huang transforms of pressure signals. The resonant intermittency was observed for a shallow cavity flow.
Original language | English |
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Pages (from-to) | 237-244 |
Number of pages | 8 |
Journal | Journal of Aeronautics, Astronautics and Aviation |
Volume | 41 |
Issue number | 4 |
Publication status | Published - 2009 Dec |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science