超音速ノズルにおける乱流境界層の発達
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概要
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The effects of velocity profile and local skin friction coefficient on the turbulent boundary-1ayer development in a supersonic nozzle were investigated by using Tucker's method. The calculated results agree well with the experimental data in zero－and favorable pressure gradient flows provided that the pertinent velocity profile parameter and the local skin friction coefficient are selected. Also, it is shown that the turbulent boundary-layer development in the flow of which pressure gradient is almost negligible depends strongly on the local skin friction coefficient and it is almost independent on the velocity profile.
- 九州大学大学院総合理工学研究科の論文
- 1994-12-01
九州大学大学院総合理工学研究科 | 論文
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