摘要
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.
原文 | English |
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頁(從 - 到) | 237-244 |
頁數 | 8 |
期刊 | Journal of Aeronautics, Astronautics and Aviation |
卷 | 41 |
發行號 | 4 |
出版狀態 | Published - 2009 12月 |
All Science Journal Classification (ASJC) codes
- 航空工程
- 空間與行星科學