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Richard,
What software did you use to design the aircraft? The aircraft looks pretty damn good. Jim Williams UOTE=Richard Lamb]Well, since you asked... this one is a 76 sq. ft wing which is not the exact right wing for this plane, but the worksheet was already done-so...what. No idea how the columns will hold up on the net, but ..... it's worth a try... The spar caps are 1-1/5" X 1/8" 6061 with 1-1/2" x 1/8" 6061 straps layered to the indicated (interpreted) thickness. Bruce bolted his spar, which produced a very straight spar assembly. Hammering big rivets into small structures will invariably induce some distortion. We are doing is a beam spar rather than a proper box, so the sheer web dimension should be doubled. And? No promise that any of this is close to correct... ================================================== ====================== X-Wing SPAR Build .58 R.Lamb 2001 Project Name L-One V Run time: 01-10-2006 at 10:43:10 Wing Span [ft] 17.00 Root Chord [ft] 5.00 Wing Area [sqft] 76.50 Tip Chord [ft] 4.00 Chord thickness [%] 12.00 Mean Chord [ft] 4.50 Gross Wgt [lb] 888.00 Aspect Ratio [#] 3.78 Lift (Vs) [lb] 888.00 Wing Loading [lb/sqft] 11.61 V(min) [mph] 59.04 Max CL [#] 1.30 Load Factor [G's] 4.00 Spar Width [inches] 1.50 Cap Compression [psi] 66,000 Shear Web [psi] 10,000 Thickness [% of Chord] 12 Sta W.STA. AIR LOAD SHEAR MOM FTLB num FT PPF LB FT.LB 1 0.000 232.000 1776.000 7268.000 2 0.850 236.000 1580.000 5842.000 3 1.700 241.000 1389.000 4580.000 4 2.550 246.000 1201.000 3479.000 5 3.400 250.000 1018.000 2536.000 6 4.250 255.000 838.000 1747.000 7 5.100 260.000 663.000 1109.000 8 5.950 264.000 491.000 618.000 9 6.800 269.000 323.000 272.000 10 7.650 273.000 159.000 67.000 11 8.500 278.000 0.000 -1.000 Spar weight parameters: Sta W.Sta. SPAR HGT CAP THK WEB THK num FT IN IN IN 1 0.000 5.760 0.306 0.031 2 0.850 5.645 0.251 0.028 3 1.700 5.530 0.201 0.025 4 2.550 5.414 0.156 0.022 5 3.400 5.299 0.116 0.019 6 4.250 5.184 0.082 0.016 7 5.100 5.069 0.053 0.013 8 5.950 4.954 0.030 0.010 9 6.800 4.838 0.014 0.007 10 7.650 4.723 0.003 0.003 11 8.500 4.608 -0.000 0.000 Shear web thickness is for a box type spar. For single web, double it. ================================================== ======================[/quote] |
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