低マッハ数超音速流れにおける擬似衝撃波の振動
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概要
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The oscillatory characteristics of a pseudo-shock wave with an incoming Mach number of 1.75 in a rectangular straight duct are experimentally investigated by static pressure measurements both on the duct axis and on the wall surface. Statistical analysis is applied to the detailed fluctuating pressure data in the pseudo-shock region. The correlation between the oscillatory characteristics and the flow mechanism of the pseudo-shock wave is also discussed in detail in the last part of the present paper.
- 九州大学大学院総合理工学研究科の論文
- 1991-06-01
九州大学大学院総合理工学研究科 | 論文
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