************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file 3.28 version * ************************************************************** * Version 2021-10-10 updated to 2023-04-26, 2026-04-20 * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "gnuC2-27" * Drawing scale 1.5 * Wing scale 1.03468783 * Number of cells 60 * Number of ribs 61 * Alpha wingtip, parameter, (alpha center) 6.0 2 0.0 * Paraglider type and parameter "ds" 0 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin Rot_z Pos_z 1 .00 .00 246.74 .00 .00 .00 33.33 .00 0.00 50.0 2 25.06 .14 246.71 25.05 .48 2.16 33.33 .00 0.17 50.0 3 50.08 .56 246.60 50.03 1.90 4.42 33.33 .00 0.35 50.0 4 75.04 1.25 246.43 74.88 4.25 6.49 33.33 .00 0.51 50.0 5 99.91 2.23 246.20 99.53 7.53 8.75 33.33 .00 0.68 50.0 6 124.68 3.48 245.89 123.94 11.72 10.81 33.33 .00 0.84 50.0 7 149.30 5.01 245.52 148.04 16.78 12.88 33.33 .00 1.00 50.0 8 173.77 6.81 245.09 171.78 22.69 15.14 33.33 .00 1.17 50.0 9 198.06 8.90 244.59 195.11 29.43 17.21 33.33 .00 1.33 50.0 10 222.13 11.27 244.02 217.98 36.96 19.34 33.33 .00 1.49 50.0 11 245.97 13.93 243.40 240.30 45.34 21.81 33.33 .00 1.67 50.0 12 269.56 16.87 242.71 262.00 54.56 24.28 33.33 .00 1.85 50.0 13 292.86 20.10 241.96 283.04 64.57 26.55 33.33 .00 2.01 50.0 14 315.85 23.62 241.16 303.38 75.30 29.02 33.33 .00 2.18 50.0 15 338.51 27.44 240.29 322.97 86.68 31.28 33.33 .00 2.34 50.0 16 360.82 31.56 239.38 341.78 98.66 33.54 33.33 .00 2.49 50.0 17 382.74 35.98 238.41 359.79 111.15 35.81 33.33 .00 2.63 50.0 18 404.24 40.73 237.39 376.97 124.09 38.07 33.33 .00 2.77 50.0 19 425.32 45.80 236.32 393.27 137.44 40.74 33.33 .00 2.94 50.0 20 445.92 51.28 235.22 408.56 151.25 43.54 33.33 .00 3.10 50.0 21 466.00 57.44 234.07 422.78 165.42 46.19 33.33 .00 3.25 50.0 22 485.51 64.31 232.89 435.94 179.83 49.00 33.33 .00 3.40 50.0 23 504.40 71.89 231.69 448.01 194.35 51.48 33.33 .00 3.52 50.0 24 522.62 80.15 230.60 459.03 208.86 54.12 33.33 .00 3.65 50.0 25 540.14 89.10 229.62 468.99 223.27 56.88 33.33 .00 3.77 50.0 26 556.91 98.74 228.73 477.72 237.58 60.31 33.33 .00 3.91 50.0 27 572.88 109.14 227.95 485.26 251.66 63.34 33.33 .00 4.02 50.0 28 588.00 120.34 227.25 491.66 265.36 66.37 33.33 .00 4.12 50.0 29 602.22 132.53 226.63 497.02 278.53 69.20 33.33 .00 4.21 50.0 30 615.43 146.04 226.08 501.41 290.99 71.83 33.33 .00 4.28 50.0 31 627.50 161.65 225.60 506.32 307.72 74.26 33.33 .00 4.33 50.0 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name. intake in. intake out. open. disp rweight 1 gnuC2.txt 4.0 6.0 1 2.0 1 1 2 gnuC2.txt 4.0 6.0 1 1.5 1 17 3 gnuC2.txt 4.0 6.0 1 0 1 17 4 gnuC2.txt 4.0 6.0 1 0 1 17 5 gnuC2.txt 4.0 6.0 1 1.0 1 17 6 gnuC2.txt 4.0 6.0 1 1.0 1 15 7 gnuC2.txt 4.0 6.0 1 0 1 15 8 gnuC2.txt 4.0 6.0 1 0 1 15 9 gnuC2.txt 4.0 6.0 1 1.5 1 15 10 gnuC2.txt 4.0 6.0 1 2.0 1 15 11 gnuC2.txt 4.0 6.0 1 1.5 1 15 12 gnuC2.txt 4.0 6.0 1 0 1 15 13 gnuC2.txt 4.0 6.0 1 0 1 15 14 gnuC2.txt 4.0 6.0 1 1.0 1 15 15 gnuC2.txt 4.0 6.0 1 1.0 1 15 16 gnuC2.txt 4.0 6.0 1 0 1 15 17 gnuC2.txt 4.0 6.0 1 0 1 15 18 gnuC2.txt 4.0 6.0 1 0.9 1 15 19 gnuC2.txt 4.0 6.0 1 0.9 1 15 20 gnuC2.txt 4.0 6.0 1 0 1 15 21 gnuC2.txt 4.0 6.0 1 0.5 1 15 22 gnuC2.txt 4.0 6.0 1 0 1 15 23 gnuC2.txt 4.0 6.0 1 0.5 1 15 24 gnuC2.txt 4.0 6.0 1 0 1 15 25 gnuC2.txt 4.0 6.0 1 0.5 1 15 26 gnuC2.txt 4.0 6.0 1 0 1 15 27 gnuC2.txt 4.0 6.0 0 0.8 1 15 28 gnuC2.txt 4.0 6.0 0 0.8 1 15 29 gnuC2.txt 4.0 6.0 0 0 1 15 30 gnuC2.txt 4.0 6.0 0 0 1 15 31 gnuC2.txt 4.0 6.0 0 0 1 1 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 3 10 37 72 0 0 0 2 3 10 37 72 0 0 0 3 3 10 37 72 0 0 100 4 3 10 37 72 0 0 100 5 3 10 37 72 0 0 100 6 3 10 37 72 0 0 100 7 3 10 37 72 0 0 100 8 3 10 37 72 0 0 100 9 3 10 37 72 0 0 100 10 3 10 37 72 0 0 100 11 3 10 37 72 0 0 100 12 3 10 37 72 0 0 100 13 3 10 37 72 0 0 100 14 3 10 37 72 0 0 100 15 3 10 37 72 0 0 100 16 3 10 37 72 0 0 100 17 3 10 37 72 0 0 100 18 3 10 37 72 0 0 100 19 3 10 37 72 0 0 100 20 3 10 37 72 0 0 100 21 3 10 37 72 0 0 100 22 3 10 37 72 0 0 100 23 3 10 37 72 0 0 100 24 3 10 37 72 0 0 100 25 3 10 37 72 0 0 100 26 3 10 37 72 0 0 100 27 3 10 37 72 0 0 100 28 3 10 37 72 0 0 100 29 3 10 37 72 0 0 100 30 3 10 37 72 0 0 100 31 3 5. 40 77 0 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 7 1 1 9 1 14.69 2.40 2.00 5.3 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 2.40 2.05 5.3 0. 0. 0. 0. 1 42.5 1.52 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 2 2 9 1 14.69 -0.39 2.05 4.06 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 0.59 2.05 5.3 0. 0. 0. 0. 1 42.5 -0.45 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 3 8 9 1 14.69 2.40 2.00 5.3 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 2.40 2.05 5.3 0. 0. 0. 0. 1 42.5 1.52 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 9 9 9 1 14.69 -0.39 2.05 4.06 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 0.59 2.05 5.3 0. 0. 0. 0. 1 42.5 -0.45 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 10 10 9 1 14.69 2.40 2.00 5.3 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 2.40 2.05 5.3 0. 0. 0. 0. 1 42.5 1.52 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 11 11 9 1 14.69 -0.39 2.05 4.06 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 0.59 2.05 5.3 0. 0. 0. 0. 1 42.5 -0.45 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. 12 30 9 1 14.69 2.40 2.00 5.3 0. 0. 0. 0. 1 22.0 2.40 3.07 7.15 0. 0. 0. 0. 1 29.3 2.40 2.05 5.3 0. 0. 0. 0. 1 42.5 1.52 2.05 3.82 0. 0. 0. 0. 1 50.0 1.52 2.84 5.89 0. 0. 0. 0. 1 57.48 1.52 2.05 3.82 0. 0. 0. 0. 1 64.80 0.75 2.05 2.8 0. 0. 0. 0. 1 78.7 0.53 1.62 1.62 0. 0. 0. 0. 1 84.4 0.25 1.47 1.47 0. 0. 0. 0. ************************************************************* * 5. SKIN TENSION * ************************************************************* Extrados 0. 0.0 0. 0. 7.5 1.3 10. 1.33 15. 2.5 20. 2.5 80. 2.5 80. 2.5 90. 1.33 90. 1.33 100. 0.0 100. 0. 0.0114 1000 1.0 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 12 22 22 upper panels (mm) 12 22 22 lower panels (mm) 12 ribs (mm) 12 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.5 0.15 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 10.5 * Plumb point % of chord 38 * Calage % 33 * Risers lenght cm 47 * Line lenght cm (without risers) 708 * Karabiners cm 42 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 3 12 4 1 1 2 1 3 1 4 1 1 3 4 1 1 2 1 3 1 4 2 1 4 4 1 1 2 1 3 2 4 3 1 7 4 1 1 2 1 3 2 4 4 1 8 4 1 1 2 2 3 3 4 5 1 12 4 1 1 2 2 3 3 4 6 1 13 4 1 1 2 2 3 4 4 7 1 16 4 1 1 2 2 3 4 4 8 1 17 4 1 1 2 3 3 5 4 9 1 20 4 1 1 2 3 3 5 4 10 1 22 4 1 1 2 3 3 6 4 11 1 24 4 1 1 2 3 3 6 4 12 1 26 12 4 1 1 2 1 3 1 4 1 2 3 4 1 1 2 1 3 1 4 2 2 4 4 1 1 2 1 3 2 4 3 2 7 4 1 1 2 1 3 2 4 4 2 8 4 1 1 2 2 3 3 4 5 2 12 4 1 1 2 2 3 3 4 6 2 13 4 1 1 2 2 3 4 4 7 2 16 4 1 1 2 2 3 4 4 8 2 17 4 1 1 2 3 3 5 4 9 2 20 4 1 1 2 3 3 5 4 10 2 22 4 1 1 2 3 3 6 4 11 2 24 4 1 1 2 3 3 6 4 12 2 26 18 4 1 1 2 1 3 1 4 1 3 3 4 1 1 2 1 3 1 4 2 3 4 4 1 1 2 1 3 2 4 3 3 7 4 1 1 2 1 3 2 4 4 3 8 4 1 1 2 2 3 3 4 5 3 12 4 1 1 2 2 3 3 4 6 3 13 4 1 1 2 2 3 4 4 7 3 16 4 1 1 2 2 3 4 4 8 3 17 4 1 1 2 3 3 5 4 9 3 20 4 1 1 2 3 3 5 4 10 3 22 4 1 1 2 3 3 6 4 11 3 24 4 1 1 2 3 3 6 4 12 3 26 3 1 1 2 4 3 7 0 0 1 29 3 1 1 2 4 3 8 0 0 1 31 3 1 1 2 4 3 9 0 0 2 29 3 1 1 2 4 3 10 0 0 2 31 3 1 1 2 4 3 11 0 0 3 29 3 1 1 2 4 3 12 0 0 3 31 *************************************************** * 10. BRAKES *************************************************** 300 12 4 1 1 2 1 3 1 4 1 6 3.5 4 1 1 2 1 3 1 4 2 6 6 4 1 1 2 1 3 2 4 3 6 9 4 1 1 2 1 3 2 4 4 6 11 4 1 1 2 2 3 3 4 5 6 14 4 1 1 2 2 3 3 4 6 6 16 4 1 1 2 2 3 4 4 7 6 19 4 1 1 2 2 3 4 4 8 6 21 4 1 1 2 3 3 5 4 9 6 24 4 1 1 2 3 3 5 4 10 6 26 4 1 1 2 3 3 6 4 11 6 28 4 1 1 2 3 3 6 4 12 6 30 * Brake distribution 0 25 50 80 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 275 100 3 135 4 200 80 *************************************************** * 12. H V and VH ribs *************************************************** 117 70 120 1 1 1 1 2 1 5.0 0. 0. 0. 2 1 2 1 3 1 5.0 0. 0. 0. 3 1 1 2 2 2 5.0 0. 0. 0. 4 1 2 2 3 2 5.0 0. 0. 0. 5 1 1 3 2 3 5.0 0. 0. 0. 6 1 2 3 3 3 5.0 0. 0. 0. 7 6 1 10 100 18.1 18.1 2 10 70 11.2 11.2 8 6 2 10 70 11.2 11.2 3 10 0 5.0 5.0 9 6 1 37 100 20.1 20.1 2 37 70 11.2 11.2 10 6 2 37 70 11.2 11.2 3 37 0 5.0 5.0 11 6 1 72 100 18.1 18.1 2 72 70 11.2 11.2 12 6 2 72 70 11.2 11.2 3 72 0 5.0 5.0 13 6 8 10 0 5.0 5.0 9 10 70 11.2 11.2 14 6 9 10 70 11.2 11.2 10 10 100 16.1 16.1 15 6 8 37 0 5.0 5.0 9 37 70 11.2 11.2 16 6 9 37 70 11.2 11.2 10 37 100 18.1 18.1 17 6 8 72 0 5.0 5.0 9 72 70 11.2 11.2 18 6 9 72 70 11.2 11.2 10 72 100 16.1 16.1 19 6 10 10 100 16.1 16.1 11 10 70 11.2 11.2 20 6 11 10 70 11.2 11.2 12 10 0 5.0 5.0 21 6 10 37 100 18.1 18.1 11 37 70 11.2 11.2 22 6 11 37 70 11.2 11.2 12 37 0 5.0 5.0 23 6 10 72 100 16.1 16.1 11 72 70 11.2 11.2 24 6 11 72 70 11.2 11.2 12 72 0 5.0 5.0 25 6 4 10 0.0 5.0 5.0 5 10 100 16.1 16.1 26 6 4 37 0.0 5.0 5.0 5 37 100 18.1 18.1 27 6 4 72 0.0 5.0 5.0 5 72 100 16.1 16.1 28 6 6 10 100 16.1 16.1 7 10 0 5.0 5.0 29 6 6 37 100 18.1 18.1 7 37 0 5.0 5.0 30 6 6 72 100 16.1 16.1 7 72 0 5.0 5.0 31 6 13 10 0.0 5.0 5.0 14 10 100 16.1 16.1 32 6 13 37 0.0 5.0 5.0 14 37 100 16.1 16.1 33 6 13 72 0.0 5.0 5.0 14 72 100 16.1 16.1 34 6 15 10 100 16.1 16.1 16 10 0 5.0 5.0 35 6 15 37 100 16.1 16.1 16 37 0 5.0 5.0 36 6 15 72 100 16.1 16.1 16 72 0 5.0 5.0 37 6 17 10 0.0 5.0 5.0 18 10 100 16.1 16.1 38 6 17 37 0.0 5.0 5.0 18 37 100 16.1 16.1 39 6 17 72 0.0 5.0 5.0 18 72 100 16.1 16.1 40 6 19 10 100 16.1 16.1 20 10 0 5.0 5.0 41 6 19 37 100 16.1 16.1 20 37 0 5.0 5.0 42 6 19 72 100 16.1 16.1 20 72 0 5.0 5.0 43 3 20 1 0 1 5.0 10.1 0. 0. 44 3 20 2 0 1 5.0 10.1 0. 0. 45 3 20 3 0 1 5.0 10.1 0. 0. 46 3 22 1 1 1 5.0 10.1 0. 0. 47 3 22 2 1 1 5.0 10.1 0. 0. 48 3 22 3 1 1 5.0 10.1 0. 0. 49 3 24 1 1 1 5.0 10.1 0. 0. 50 3 24 2 1 1 5.0 10.1 0. 0. 51 3 24 3 1 1 5.0 10.1 0. 0. 52 3 26 1 1 0 5.0 10.1 0. 0. 53 3 26 2 1 0 5.0 10.1 0. 0. 54 3 26 3 1 0 5.0 10.1 0. 0. 55 3 26 1 0 1 5.0 8.0 0. 0. 56 3 26 2 0 1 5.0 8.0 0. 0. 57 3 26 3 0 1 5.0 8.0 0. 0. 58 3 29 1 1 0 5.0 8.0 0. 0. 59 3 29 2 1 0 5.0 8.0 0. 0. 60 3 29 3 1 0 5.0 8.0 0. 0. 61 16 1 23.5 0.0 2.5 2.5 2 23.5 0.0 2.5 2.5 62 16 2 23.5 0.0 2.5 2.5 3 23.5 0.0 2.5 2.5 63 16 3 23.5 0.0 2.5 2.5 4 23.5 0.0 2.5 2.5 64 16 4 23.5 0.0 2.5 2.5 5 23.5 0.0 2.5 2.5 65 16 5 23.5 0.0 2.5 2.5 6 23.5 0.0 2.5 2.5 66 16 6 23.5 0.0 2.5 2.5 7 23.5 0.0 2.5 2.5 67 16 7 23.5 0.0 2.5 2.5 8 23.5 0.0 2.5 2.5 68 16 8 23.5 0.0 2.5 2.5 9 23.5 0.0 2.5 2.5 69 16 9 23.5 0.0 2.5 2.5 10 23.5 0.0 2.5 2.5 70 16 10 23.5 0.0 2.5 2.5 11 23.5 0.0 2.5 2.5 71 16 11 23.5 0.0 2.5 2.5 12 23.5 0.0 2.5 2.5 72 16 12 23.5 0.0 2.5 2.5 13 23.5 0.0 2.5 2.5 73 16 13 23.5 0.0 2.5 2.5 14 23.5 0.0 2.5 2.5 74 16 14 23.5 0.0 2.5 2.5 15 23.5 0.0 2.5 2.5 75 16 15 23.5 0.0 2.5 2.5 16 23.5 0.0 2.5 2.5 76 16 16 23.5 0.0 2.5 2.5 17 23.5 0.0 2.5 2.5 77 16 17 23.5 0.0 2.5 2.5 18 23.5 0.0 2.5 2.5 78 16 18 23.5 0.0 2.5 2.5 19 23.5 0.0 2.5 2.5 79 16 19 23.5 0.0 2.5 2.5 20 23.5 0.0 2.5 2.5 80 16 20 23.5 0.0 2.5 2.5 21 23.5 0.0 2.5 2.5 81 16 21 23.5 0.0 2.5 2.5 22 23.5 0.0 2.5 2.5 82 16 22 23.5 0.0 2.5 2.5 23 23.5 0.0 2.5 2.5 83 16 1 54.5 0.0 2.5 2.5 2 54.5 0.0 2.5 2.5 84 16 2 54.5 0.0 2.5 2.5 3 54.5 0.0 2.5 2.5 85 16 3 54.5 0.0 2.5 2.5 4 54.5 0.0 2.5 2.5 86 16 4 54.5 0.0 2.5 2.5 5 54.5 0.0 2.5 2.5 87 16 5 54.5 0.0 2.5 2.5 6 54.5 0.0 2.5 2.5 88 16 6 54.5 0.0 2.5 2.5 7 54.5 0.0 2.5 2.5 89 16 7 54.5 0.0 2.5 2.5 8 54.5 0.0 2.5 2.5 90 16 8 54.5 0.0 2.5 2.5 9 54.5 0.0 2.5 2.5 91 16 9 54.5 0.0 2.5 2.5 10 54.5 0.0 2.5 2.5 92 16 10 54.5 0.0 2.5 2.5 11 54.5 0.0 2.5 2.5 93 16 11 54.5 0.0 2.5 2.5 12 54.5 0.0 2.5 2.5 94 16 12 54.5 0.0 2.5 2.5 13 54.5 0.0 2.5 2.5 95 16 13 54.5 0.0 2.5 2.5 14 54.5 0.0 2.5 2.5 96 16 14 54.5 0.0 2.5 2.5 15 54.5 0.0 2.5 2.5 97 16 15 54.5 0.0 2.5 2.5 16 54.5 0.0 2.5 2.5 98 16 16 54.5 0.0 2.5 2.5 17 54.5 0.0 2.5 2.5 99 16 17 54.5 0.0 2.5 2.5 18 54.5 0.0 2.5 2.5 100 16 18 54.5 0.0 2.5 2.5 19 54.5 0.0 2.5 2.5 101 16 19 54.5 0.0 2.5 2.5 20 54.5 0.0 2.5 2.5 102 16 20 54.5 0.0 2.5 2.5 21 54.5 0.0 2.5 2.5 103 16 21 54.5 0.0 2.5 2.5 22 54.5 0.0 2.5 2.5 104 16 22 54.5 0.0 2.5 2.5 23 54.5 0.0 2.5 2.5 105 16 1 80.0 0.0 2.0 2.0 2 80.0 0.0 2.0 2.0 106 16 2 80.0 0.0 2.0 2.0 3 80.0 0.0 2.0 2.0 107 16 3 80.0 0.0 2.0 2.0 4 80.0 0.0 2.0 2.0 108 16 4 80.0 0.0 2.0 2.0 5 80.0 0.0 2.0 2.0 109 16 5 80.0 0.0 2.0 2.0 6 80.0 0.0 2.0 2.0 110 16 6 80.0 0.0 2.0 2.0 7 80.0 0.0 2.0 2.0 110 16 7 80.0 0.0 2.0 2.0 8 80.0 0.0 2.0 2.0 112 16 8 80.0 0.0 2.0 2.0 9 80.0 0.0 2.0 2.0 113 16 9 80.0 0.0 2.0 2.0 10 80.0 0.0 2.0 2.0 114 16 10 80.0 0.0 2.0 2.0 11 80.0 0.0 2.0 2.0 115 16 11 80.0 0.0 2.0 2.0 12 80.0 0.0 2.0 2.0 116 16 12 80.0 0.0 2.0 2.0 13 80.0 0.0 2.0 2.0 117 16 13 80.0 0.0 2.0 2.0 14 80.0 0.0 2.0 2.0 ***************************************************** * 15. Extrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 16. Intrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 17. Aditional rib points ***************************************************** 0 ***************************************************** * 18. Elastic lines corrections ***************************************************** 100 75 25 40 40 20 35 35 20 10 35 35 15 10 5 1 0.08 0.2 0.2 2 0.08 0.2 0.2 3 0.08 0.2 0.2 4 0.08 0.2 0.2 5 0.08 0.2 0.2 ****************************************************** * 19. DXF layer names ****************************************************** 10 general default line-external cutexternal line-sewing cutinternal points points circles circles triangles triangle square square text text reference refer notes notes ****************************************************** * 20. Marks types ****************************************************** 10 typepoint 1 1.2 1.2 2 0.3 1.2 typepoint2 1 0.25 1.2 2 0.2 1.2 typepoint3 1 0.25 1.2 2 0.2 1.2 typevent 1 10. 0.0 2 2.0 0.0 typetab 1 10. 0.0 3 2.0 0.0 typejonc 1 10. 0.0 2 2.0 0.0 typeref 1 5.0 1. 1 2.0 0.0 type8 1 0.2 5.0 1 0.0 5.0 type9 1 0.0 7.0 1 3.2 4.5 type10 1 0.0 6.0 1 0.0 3.33 ******************************************************* * 21. JONCS DEFINITION (NYLON RODS) ******************************************************* 2 1 1 3 1 1 1 30 4.2 10.8 1.0 2.0 3.5 5.0 1.0 0.7 4.5 5.0 2.2 1.0 3.67 12.1 0.79 2.0 0.0 10.35 6.3 9.35 ******************************************************* * 22. NOSE MYLARS DEFINITION ******************************************************* 0 ******************************************************* * 23. TAB REINFORCEMENTS ******************************************************* 0 ******************************************************* * 24. GENERAL 2D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 30 orange C_lines_color 3 green D_lines_color 4 cyan E_lines_color 6 magenta F_lines_color 5 blue ******************************************************* * 25. GENERAL 3D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 8 grey C_lines_color 8 grey D_lines_color 8 grey E_lines_color 8 grey F_lines_color 30 orange Extrados 1 5 blue Vents 0 1 red Intrados 1 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 10 0 11 0 12 0 13 0 14 0 15 0 16 0 17 0 18 0 19 0 20 0 21 0 22 0 23 0 24 0 25 0 26 0 27 -2 28 -1 29 -1 30 -1 31 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 3 10. 37. 72. 0 0 0 -4 20 4 20 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 31 upper 1 1 1 63 73 0.0 lower 0 1 * Print parameters Inter3D 1 1 31 0 Ovali3D 1 1 31 0 tesse3D 1 1 1 0 exteDXF 0 1 1 0 exteSTL 1 1 31 1 ******************************************************* * 30. AIRFOIL THICKNESS MODIFICATION ******************************************************* 1 1 1.0 2 1.0 3 1.0 4 1.0 5 1.0 6 1.0 7 1.0 8 1.0 9 1.0 10 1.0 11 1.0 12 1.0 13 1.0 14 1.0 15 1.0 16 1.0 17 1.0 18 1.0 19 1.0 20 1.0 21 1.0 22 1.0 23 1.0 24 1.0 25 1.0 26 1.0 27 1.0 28 1.0 29 1.0 30 1.0 31 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 31, 10 points, type "1" 1 1 31 10 1 1 0. 0.0 0. 0. 2 3.75 0.5 5. 0.665 3 7.5 1.2 10. 1.33 4 11.25 1.83 15. 1.95 5 15. 2.19 20. 2.32 6 25. 2.5 25. 2.5 7 72. 2.5 75. 2.5 8 80. 2.2 80. 2.2 9 90. 1.33 90. 1.3 10 100. 0.0 100. 0. ******************************************************* * 32. PARAMETERS FOR PARTS SEPARATION ******************************************************* 1 panel_x 1.2 panel_x_min 1.0 panel_y 0.8 rib_x 0.8 rib_y 1.0 rib_1y 1.8 jonc_x 1.0 jonc_y 1.0 jonc_i 0.0 parameter10 1.0 ******************************************************* * 33. DETAILED RISERS ******************************************************* 1 1 A 47.0 cm B 47.0 cm C 47.0 cm ******************************************************* * 34. LINES CHARACTERISTICS TABLE ******************************************************* 1 6 1 c 5.0 Riser 1000 daN u_dyneem 10.0 g p 12. cm 7 2 c 1.90 Line275 275 daN s_dyneem 2.26 g s 12. cm 1 3 c 1.40 Line160 160 daN s_dyneem 1.34 g s 10. cm 3 4 c 1.15 Line120 120 daN s_dyneem 1.00 g s 10. cm 5 5 c 0.80 Line100U 100 daN u_dyneem 0.43 g p 8. cm 2 6 c 2.00 Line200B 200 daN s_dynemm 3.10 g s 12. cm 6 ******************************************************* * 35. SOLVE EQUILIBRIUM EQUATIONS ******************************************************* 1 g 9.807 m/s2 gravity of Earth ro 1.225 kg/m3 air mass density mu 18.46 muPa·s air dynamic viscosity (microPascals) V 12.4 m/s estimated flow speed Alpha 9.45 deg estimated wing angle of attact at trim speed Cl 0.67913 wing lift coefficient cle 1.0 lift correction coefficient Cd 0.03790 wing drag coefficient cde 1.1 drag correction coefficient Cm 0.0 wing moment coefficient Spilot 0.438 m2 pilot+harness frontal surface Cdpilot 0.6 pilot+harness drag coefficient Mw 4.0 kg wing mass Mp 70 kg pilot mass included harness and instruments Pmc 0.2 m pilot mass center below main karabiners Mql 8.0 g one quick link mass (riser-lines) Ycp 0.575 m y-coordinate center of pressure Zcp 0.395 m z-coordinate center of pressure ******************************************************* * 36. CREATE FILES FOR XFLR5 ANALYSIS ******************************************************* 1 * Panel parameters 10 chord nr 5 per cell 1 cosine distribution along chord 0 uniform along span * Include billowed airfoils (more accuracy) 0 ******************************************************* * 37. SOME SPECIAL PARAMETERS ******************************************************* 1 6 1291 8 nsegments in transverse direction (stl surfaces) 1341 0 use CAD colors for each line type according table 34 1146 36. gravity center in % of a typical section (default is 36%) 1351 1 Solve method (1 or 6) 1352 2 Use flat area (1) or projected area (2) 1353 2 Print normal (0) or advanced detailed output (1),(2)