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Old 11-20-2005 | 06:02 PM
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BWooster
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From: Edmonton, AB,
Default RE: Wing affect on horizontal stab
Judging from the graph, I make the centreline of the wake at roughly 4.5" below the wing TE with lift coefficient of 1.

The angle of the downwash at level with TE is about 5 degrees, if I'm reading this correctly.
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