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Search: Posts Made By: bookworm
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Forum: Tech Log
25th Feb 2010, 17:20
Replies: 5
Views: 1,478
Posted By bookworm

Yes. If you have a look at the drag polars of...

Yes. If you have a look at the drag polars of aerofoils (rather than finite wings), you still see a roughly quadratic dependence on lift coefficient (i.e. on AoA). For cambered wings, the minimum...
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