Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence (Q1925215)
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scientific article; zbMATH DE number 939565
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence |
scientific article; zbMATH DE number 939565 |
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Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence (English)
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17 March 1997
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The combined influence of the second-approximation effects in three-dimensional unseparated flow over long blunt cones is investigated. The solution over the entire domain between the surface of the body and the surface of the shock wave, including subsonic flow regions, is found in a unified manner using a numerical method based on global iterations.
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long blunt cones
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numerical method
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global iterations
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0.85238624
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0.8509129
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0.8502351
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0.8463013
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0.83852243
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0.83758545
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0.8332943
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