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From: Jason Werner (jwerner@oleen.com)
Date: Fri 25 Apr 2003 - 05:45:18 BST
Alan,
Something seems too simple here. For example, where does the coeff of
lift of that particular planform come into play? I know for a fact that
different airfoils produce different amounts of lift at the same AoA. So to
me that would indicate that different setups should account for that. Are
you indicting a zero lift airfoil (flat plate)? Or at least a constant in
that regards?
Just curious
Jason Werner
----- Original Message -----
From: "Alan Smith" <alans@arcom.com.au>
To: "Jason Werner" <jwerner@oleen.com>; <14list@i14.org>
Sent: Thursday, April 24, 2003 7:11 AM
Subject: Re: [I14] leeway angles = AOA
> some typical numbers
> no weather helm
>
> boat speed 3 knts c of g 0.75 ft to windward of c of b, auw 500 lbs,
> distance from c of e sails to c of e cb 11 ft, force on cb 500 X 0.75 / 11
=
> 56.8 lbs, leeway angle 4.7 degrees
> boat speed 8 knots, c of g 5 ft to windward of c of b, force 227 lbs
leeway
> angle 2.6 degrees
>
> a cb area of 3 square ft has been used in these calculation...leeway angle
> is inversely proportional to cb area and the square of boat speed ..run
your
> own estimates from the base provided above
>
>
>
> the force on the centre board also induces a drag component which is
> approximately the force times SIN (leeway angle/2) so it is important to
> keep the leeway angle small by using sufficient cb area for the conditions
> of the day
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