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Structural Testing Of Homebuilt Aircraft
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Structural Testing Of Homebuilt Aircraft

Manhattan Dr. reaches a huge value of some 0.12 or questions, will nevertheless tell the Tempe, AZ 85282 12%. This value of the strain is so far builder a great deal about the out to the right it does not even show strength and the structural integrity in Figure 1. Similar behavior can be of his aircraft. It will also contribue straight lines). Twice the stress, twice observed on a tensile specimen of a to his peace of mind. the strain. The behavior of the certified spruce (yield point around Let us start by pausing briefly to stretched aluminum alloy (20 24 -T3), 5.3 ksi, ultimate strength about 9.4 consider a peculiar mechanical prop- spruce, or 4130 steel (not shown) is, ksi), or a low carbon steel, or CrMo erty of composite materials

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