Computer analysis of wing design for general aviation aircraft
The calculation of the two dimensional viscous incompressible flow about single and multielement aerofoil sections is considered. A panel method, based on vorticity and source distributions is used for the calculation of the potential flow. Once the velocity distribution is known, integral boundary...
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| Format: | Default OER |
| Published: |
1981
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| Online Access: | https://hdl.handle.net/2134/16174 |
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