In this case, the aspect ration increases helping to lower the drag, and
the reynolds number remains constant so you won't lose here. The longer
wing with more area will reduce the wing loading. What's the question
again? Performance should increase..
.........bc ([EMAIL PROTECTED]
http://www.widomaker.com/~conk
Williamsburg, VA 23185
On Tue, 12 Feb 2002, Jon Stone wrote:
>
> ----- Original Message -----
> From: "Bill Conkling" <[EMAIL PROTECTED]>
>
>
> > are you assuming equal aspect ratio?
>
> no. Just stretch the wing. More area from the resulting stretch. Root rib
> remains the same.
>
>
> Say just scale the panel break locations by multiplying by 130 / 118 or
> similar for a desired span.
>
> Jon
>
>
>
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