A computational study of the effect of angles of attack on a double-cone type supersonic inlet with a bleeding system (Q365519)
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scientific article; zbMATH DE number 6204851
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | A computational study of the effect of angles of attack on a double-cone type supersonic inlet with a bleeding system |
scientific article; zbMATH DE number 6204851 |
Statements
A computational study of the effect of angles of attack on a double-cone type supersonic inlet with a bleeding system (English)
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4 September 2013
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supersonic inlet
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angle of attack
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bleeding system
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AIP (Aerodynamic Interface Plane)
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0.7368217706680298
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0.7367165088653564
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