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October 2000

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Re: your mail
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AIAA Student Design/Build/Fly Competition Project <[log in to unmask]>
Date:
Fri, 27 Oct 2000 07:08:59 -0500
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TEXT/PLAIN (35 lines) 
That is a 75% decrease in the Y axis for the CLARK Y and a 79% decrease in
the SD7062 so that the max thickness for each airfoil will be 2 inches-the
thickness of the blue foam.

RCW

 On Thu, 26 Oct 2000, Tyler Martin wrote:

> Steve & Tommy-
> Doc wants us to increase the cordinate size of the airfoils by the following
> amounts:
> Clark YM-15:
> Y axis= 75% increase
> x axis= to 18 inches
>
> SD7062
> Y axis= 79% increase
> X axis= to 18 inches
>
> These two airfoils will be our best bet because they give us a bit more
> thickness than the others; giving it more strength.  I know you all were
> planning on cutting out the plates on the 27th; if someone could post a time
> that would be great.
>
> Tyler
>
> P.S.
> ..and Peter if you could get those TPS reports to me that would be Grrreeeaat.
> Lumberg
>
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