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On Tue, 10 Jan 2006 11:24:24 GMT, Matt Whiting wrote:
Ron Wanttaja wrote: I have to admit he does bring up a good point. I have often wondered what the difference in strength's and weakness would be if I used different wood in my plane, or enlarged the components for a larger pilot. Which is probably one reasons designers don't provide the equations. Many hate it when folks make changes. Most equations for light airplane design are well established and have been around for decades. What unique equations could a typical designer provide? Not the equations per se, but the precise values and the design margins of the design in question, the non-designer's lack of understanding of the interrelationships between design elements, and the legal implications of *providing* the information. Remember, the poster I responded to specifically referred to the substitution of one material for another. It's sometimes more than a mere comparison of the strengths of the materials. Ron Wanttaja |
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