************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file 2.60 version * ************************************************************** * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "gnu-C" * Drawing scale 1.5 * Wing scale 1.0 * 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 1 .00 .00 246.74 .00 .00 .00 33.33 .00 2 25.06 .14 246.71 25.05 .48 2.16 33.33 .00 3 50.08 .56 246.60 50.03 1.90 4.42 33.33 .00 4 75.04 1.25 246.43 74.88 4.25 6.49 33.33 .00 5 99.91 2.23 246.20 99.53 7.53 8.75 33.33 .00 6 124.68 3.48 245.89 123.94 11.72 10.81 33.33 .00 7 149.30 5.01 245.52 148.04 16.78 12.88 33.33 .00 8 173.77 6.81 245.09 171.78 22.69 15.14 33.33 .00 9 198.06 8.90 244.59 195.11 29.43 17.21 33.33 .00 10 222.13 11.27 244.02 217.98 36.96 19.34 33.33 .00 11 245.97 13.93 243.40 240.30 45.34 21.81 33.33 .00 12 269.56 16.87 242.71 262.00 54.56 24.28 33.33 .00 13 292.86 20.10 241.96 283.04 64.57 26.55 33.33 .00 14 315.85 23.62 241.16 303.38 75.30 29.02 33.33 .00 15 338.51 27.44 240.29 322.97 86.68 31.28 33.33 .00 16 360.82 31.56 239.38 341.78 98.66 33.54 33.33 .00 17 382.74 35.98 238.41 359.79 111.15 35.81 33.33 .00 18 404.24 40.73 237.39 376.97 124.09 38.07 33.33 .00 19 425.32 45.80 236.32 393.27 137.44 40.74 33.33 .00 20 445.92 51.28 235.22 408.56 151.25 43.54 33.33 .00 21 466.00 57.44 234.07 422.78 165.42 46.19 33.33 .00 22 485.51 64.31 232.89 435.94 179.83 49.00 33.33 .00 23 504.40 71.89 231.69 448.01 194.35 51.48 33.33 .00 24 522.62 80.15 230.60 459.03 208.86 54.12 33.33 .00 25 540.14 89.10 229.62 468.99 223.27 56.88 33.33 .00 26 556.91 98.74 228.73 477.72 237.58 60.31 33.33 .00 27 572.88 109.14 227.95 485.26 251.66 63.34 33.33 .00 28 588.00 120.34 227.25 491.66 265.36 66.37 33.33 .00 29 602.22 132.53 226.63 497.02 278.53 69.20 33.33 .00 30 615.43 146.04 226.08 501.41 290.99 71.83 33.33 .00 31 627.50 161.65 225.60 506.32 307.72 74.26 33.33 .00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name. intake in. intake out. open. disp rweight 1 gnuC-c1.txt 4.0 6.0 1 0 1 17 2 gnuC-c1.txt 4.0 6.0 1 0 1 17 3 gnuC-c1.txt 4.0 6.0 1 0 1 17 4 gnuC-c1.txt 4.0 6.0 1 0 1 17 5 gnuC-c1.txt 4.0 6.0 1 0 1 17 6 gnuC-c1.txt 4.0 6.0 1 0 1 15 7 gnuC-c1.txt 4.0 6.0 1 0 1 15 8 gnuC-c1.txt 4.0 6.0 1 0 1 15 9 gnuC-c1.txt 4.0 6.0 1 0 1 15 10 gnuC-c1.txt 4.0 6.0 1 0 1 15 11 gnuC-c1.txt 4.0 6.0 1 0 1 15 12 gnuC-c1.txt 4.0 6.0 1 0 1 15 13 gnuC-c1.txt 4.0 6.0 1 0 1 15 14 gnuC-c1.txt 4.0 6.0 1 0 1 15 15 gnuC-c1.txt 4.0 6.0 1 0 1 15 16 gnuC-c1.txt 4.0 6.0 1 0 1 15 17 gnuC-c1.txt 4.0 6.0 1 0 1 15 18 gnuC-c1.txt 4.0 6.0 1 0 1 15 19 gnuC-c1.txt 4.0 6.0 1 0 1 15 20 gnuC-c1.txt 4.0 6.0 1 0 1 15 21 gnuC-c1.txt 4.0 6.0 1 0 1 15 22 gnuC-c1.txt 4.0 6.0 1 0 1 15 23 gnuC-c1.txt 4.0 6.0 1 0 1 15 24 gnuC-c1.txt 4.0 6.0 1 0 1 15 25 gnuC-c1.txt 4.0 6.0 1 0 1 15 26 gnuC-c1.txt 4.0 6.0 1 0 1 15 27 gnuC-c1.txt 4.0 6.0 0 0 1 15 28 gnuC-c1.txt 4.0 6.0 0 0 1 15 29 gnuC-c1.txt 4.0 6.0 0 0 1 15 30 gnuC-c1.txt 4.0 6.0 0 0 1 15 31 gnuC-t.txt 0.0 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 12 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 * ************************************************************* 1 1 30 8 1 14.69 3.07 2.05 5.3 0. 0. 0. 0. 1 22.0 3.07 3.07 7.15 0. 0. 0. 0. 1 29.3 3.07 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 72.45 0.75 2.05 2.8 0. 0. 0. 0. 1 80.53 0.53 1.62 1.62 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 * Center of pressure % of chord 38 * Calage % 30 * Risers lenght cm 47 * Line lenght cm (without risers) 708 * Karabiners cm 42 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 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 *************************************************** 54 80 150 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 16.1 16.1 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 16.1 16.1 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 16.1 16.1 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 16.1 16.1 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 16.1 16.1 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 16.1 16.1 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 16.1 16.1 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 8.1 0. 0. 53 3 26 2 1 0 5.0 8.1 0. 0. 54 3 26 3 1 0 5.0 8.1 0. 0. ***************************************************** * 15. Extrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 16. Intrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 17. Aditional rib points ***************************************************** 2 7.0 8.15 12.0 -4.5 ***************************************************** * 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