Subsonic stalled flow around thin wings of delta planform (Q1803463)
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scientific article; zbMATH DE number 220906
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Subsonic stalled flow around thin wings of delta planform |
scientific article; zbMATH DE number 220906 |
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Subsonic stalled flow around thin wings of delta planform (English)
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29 June 1993
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A panel method is used to calculate the intensity of the vortices joining the wing and the free vortex sheet in the case of the subsonic flow past a triangular wing. The experimental values of the aerodynamic characteristics of the wing are compared with the values obtained numerically.
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discrete vortex method
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system of algebraic equations
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panel method
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free vortex sheet
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aerodynamic characteristics
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