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| 概要 |
The characteristics of flow field along spanwise direction induced by the interaction of weak normal shock wave with turbulent boundary layer in a supersonic nozzle were investigated experimentally. I...n the range of just upstream shock Mach number about 1.10 to 1.80, detailed time mean wall static pressure measurements were carried out along spanwise direction using multiple pressure transducers. Also, the relations between variations of upstream boundary layer and behavior of interaction flow fields were investigated. As a result, it is revealed that upstream boundary layer thickness influences the behavior of interaction somewhat for case of well-separated flow. And, another one is revealed that there is some spanwise pressure difference in unseparated flow, however, no so much difference is found in well-separated flow case.続きを見る
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