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#11
October 26th 18, 01:34 PM
posted to rec.aviation.soaring
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Electric Self Launch System
Craig,
Thanks for the advice. That is the big issue on the project. Is difficult to obtain the same rigidity of a cone like the boom tail once cut. The reinforcement floor and walls will form 3 different enclosed sections with fibers at 45° from the fuselage line. After the modifications I will test the fuselage with strain gauges to see the new strain distribution and compare them with the original. 
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