The Center of Gravity is too far back in this picture, I need to move the wing & struts a bit further back to compensate. There is no longer any tube coming down from the engine because the carbon tube should be strong enough without any support. The pilot would be wearing an aero-helmet.
Sunday, March 24, 2013
Monday, March 11, 2013
Friday, January 11, 2013
Sunday, December 9, 2012
simplified structure using rigid struts
A simpler fuselage using thick, rigid struts to take the principal flight loads in positive and negative G. The fairing is the same, it's just not shown in these images
Monday, December 3, 2012
straight line fuselage
Sunday, October 7, 2012
Sunday, June 24, 2012
Leading Edge D-Structure: 2.3 kg
3 meter long leading edge D structure, carries all flight loads for +6 -3 g. 2.3 kilograms including the fiberglass on the web faces. Will go up to 2.5 or 2.7 kilos when I include the metal fittings, and there will be about 100-200 g of glue. But it's still pretty light. Notice in the spar, the balsa wood, which is 120 kg/m3, is replaced by 28 kg/m3 foam on the outer 110 cm of the wing.
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