Calculation of two-dimensional inlet flow fields by an implicit method including viscous effects: Program documentation and test case
The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented.
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| Format: | Report |
| Sprache: | eng |
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| Zusammenfassung: | The source listing of a computer code for calculating the flow fields in a supersonic free stream is given. The application of this code to an inlet on an airbreathing missile is also presented. |
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