Experimental investigation of the weak shock wave influence on the boundary layer of a flat blunt plate at the Mach number 2.5 (Q2314589)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Experimental investigation of the weak shock wave influence on the boundary layer of a flat blunt plate at the Mach number 2.5 |
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Experimental investigation of the weak shock wave influence on the boundary layer of a flat blunt plate at the Mach number 2.5 (English)
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29 July 2019
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supersonic flow
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\(N\)-wave
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turbulence
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experiment
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boundary layer
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hot-wire anemometry
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