Brian:

Good advice!  I have had a basic course in strenth of materials and know
generally what is invoved but there are nuances(sp) and I would depend on
nothing that I did beyound the simple case and wing loadin is just not all that
simple.  Leave that to the aero engineers.

Don Lively
Burlington IA
  ------------------------------------------------------------------------

Brian Kraut wrote:

> I am not normally the one to jump in and discourage someone from trying new
> ideas, but if he does not know how to calculate the theoretical load limit
> on a simple box spar with a degree of certainty that it does not need to be
> tested under actual load and does not know the proper way to test under an
> actual load either then he should not be building his own design.
>
> That being said, there are several good books he can get on aircraft design
> and structures that do explain how to design an airplane for the intended
> loads.  More importantly, they will help him from the beginning stages of
> the design long before he needs to determine if his wings are strong enough.
> I am in New Orleans for work the rest of the week and my library is at home,
> but off the of of my head I would recommend Dan Raymer's Simplified Aircraft
> Design for Homebuilders as a must for general design and performance
> calculations although not for structural information.  Stress Without Tears
> is good.  Check the book section at www.aircraftdesign.com for others.
>
> Brian Kraut
> Engineering Alternatives, Inc.
> www.engalt.com
>
> -----Original Message-----
> From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
> Behalf Of Albert Cassar
> Sent: Wednesday, July 05, 2006 6:53 PM
> To: KRnet
> Subject: KR> Re: wing loading test
>
>     Hi all
>                A friend  would like to do a wing load test on his new
> project which is his own design. the wing spa and WAF are the same as the
> KR.
> Would he need to have the aircraft upside down and load it with sand bags or
> can it be done right side up.
> If so how do you place the bags (eg) equally over the wing or moor wight at
> the root of the wing.
>
> Thanks in advance.
> Albert
>
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