Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6 (Q2844550)
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scientific article; zbMATH DE number 6202948
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6 |
scientific article; zbMATH DE number 6202948 |
Statements
29 August 2013
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supersonic flows
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transition to turbulence
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turbulent transport
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mixing
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turbulent boundary layers
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other numerical methods
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0.8356898
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0.8259026
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0.82464164
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Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6 (English)
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Numerical investigations of an edge vortex for different values of the wing angles of attack by use the Spalart-Allmaras turbulent model are fulfield. The comparison of numerical results for different turn out flow regimes and the experimental data are provided.
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