Redesign of a supercritical wing in the presence of an engine nacelle (Q1094979)
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scientific article; zbMATH DE number 4027052
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Redesign of a supercritical wing in the presence of an engine nacelle |
scientific article; zbMATH DE number 4027052 |
Statements
Redesign of a supercritical wing in the presence of an engine nacelle (English)
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1987
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A method for modelling an engine nacelle in a compressible flow using a source distribution is described. The incorporation of this technique into a free boundary supercritical wing design code is discussed. Results of calculations made with this code are presented. A method for calculating wave drag is also described.
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modelling an engine nacelle
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compressible flow
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source distribution
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free boundary supercritical wing design code
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0.8634274
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0.84595704
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0.8302875
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0.8268955
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0.8226601
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