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Aviation > Aeronautics (aircraft design and construction) > Lift Coefficien...
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Lift Coefficient of swept wings

by GeoffS <sobering@[EMAIL PROTECTED] > May 10, 2006 at 06:17 PM

> ...However, to assume the AOA is now zero implies
> there is no change in horizontal stabilizer setting. ...

Exactly.  The point is to hold everything constant except the sweep
angle.  We're talking about why the lift/drag of a wing changes with
sweep angle, not how one might actually fly a plane with variable-sweep
wings.

Cheers,

Geoff S.
 




 1 Posts in Topic:
Lift Coefficient of swept wings
GeoffS <sobering@[EMAI  2006-05-10 18:17:33 

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