摘要
An experimental study determines the characteristics of open and transitional cylindrical cavities for compressible turbulent flow. For a given value of M, the effect of δ/cavity depth is evident only near the rear face of a cavity. The trailing-edge expansion and the amplitude of the peak pressure fluctuations decrease as δ/cavity depth increases. When the value of δ/cavity depth is less than 1.00, there is a greater decrease in the amplitude of the peak pressure fluctuations. For a given value of δ/cavity depth, the amplitude of the peak pressure fluctuations decreases as the value of M increases, particularly for a transitional cavity flow.
| 原文 | English |
|---|---|
| 頁（從 - 到） | 1564-1566 |
| 頁數 | 3 |
| 期刊 | Journal of Aircraft |
| 卷 | 53 |
| 發行號 | 5 |
| DOIs | |
| 出版狀態 | Published - 2016 |
All Science Journal Classification (ASJC) codes
- 航空工程