Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6. 80 (Q1614971)
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scientific article; zbMATH DE number 1798910
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6. 80 |
scientific article; zbMATH DE number 1798910 |
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Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6. 80 (English)
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10 September 2002
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The pressure oscillations occuring in the hypersonic flow around an axisymmetric blunt body equipped with a spike are computed by a numerical finite volume method. The numerical results are compared to experimental data, and a spectral analysis is performed.
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hypersonic flow
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separated flows
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spectral analysis
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axisymmetric blunt body
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spike
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finite volume method
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