Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow (Q1115724)
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scientific article; zbMATH DE number 4087279
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow |
scientific article; zbMATH DE number 4087279 |
Statements
Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow (English)
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1988
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The boundary layer on a semi-infinite triangular body of power-law shape is calculated for viscous interaction with an external hypersonic flow. The results of calculating the characteristics of the three-dimensional boundary layer are presented. The formation of secondary return flows and zones of intensified heat transfer on the surface of the body in the neighborhood of lines of flow divergence is noted.
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boundary layer
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semi-infinite triangular body of power-law shape
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viscous interaction
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external hypersonic flow
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three-dimensional boundary layer
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flow divergence
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0.8832475
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0.8586013
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0.85815555
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0.85719144
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0.8548143
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0.85003674
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