************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file * ************************************************************** * ************************************************************** * 1. GEOMETRY * ************************************************************** * Wing name exp * Number of cells 83 * Number of ribs 84 * Alpha max 5.2 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP 1 0.05 0.00 230.84 0.05 0.00 0.00 33.33 2 18.14 0.00 230.81 18.14 0.05 1.23 33.33 3 34.70 0.17 230.74 34.69 0.77 2.48 33.33 4 51.27 0.37 230.62 51.24 1.48 4.00 33.33 5 67.83 0.65 230.45 67.77 2.51 4.60 33.33 6 84.40 1.00 230.23 84.27 3.91 6.00 33.33 7 100.96 1.44 229.97 100.72 5.89 6.89 33.33 8 117.52 1.95 229.66 117.16 7.88 9.41 33.33 9 134.09 2.54 229.30 133.49 10.65 10.20 33.33 10 150.65 3.21 229.30 149.74 13.86 11.17 33.33 11 167.21 3.96 228.90 165.99 17.06 14.37 33.33 12 183.78 4.80 228.44 182.23 20.32 15.50 33.33 13 200.34 5.71 227.93 198.27 24.46 16.30 33.33 14 218.09 6.78 227.37 214.10 29.34 17.22 33.33 15 235.83 7.95 226.71 231.06 34.56 19.00 33.33 16 253.58 9.22 225.99 247.95 40.00 20.45 33.33 17 271.33 10.59 225.21 264.58 46.20 22.00 33.33 18 289.07 12.06 224.37 281.05 52.82 23.33 33.33 19 306.82 13.63 223.46 297.34 59.85 25.00 33.33 20 324.57 15.31 222.48 313.51 67.20 26.46 33.33 21 342.31 17.10 221.43 329.39 75.10 28.80 33.33 22 360.06 18.99 220.31 345.14 83.31 30.00 33.33 23 377.81 21.01 219.12 360.50 92.18 31.04 33.33 24 395.55 23.14 217.84 375.87 101.05 32.00 33.33 25 413.30 25.39 216.49 390.95 110.42 33.05 33.33 26 431.05 27.76 215.05 405.76 120.20 35.00 33.33 27 448.79 30.27 213.52 420.26 130.43 37.50 33.33 28 466.54 32.91 211.89 434.49 141.35 38.61 33.33 29 484.29 35.69 210.16 447.71 153.19 42.64 33.33 30 502.03 39.11 208.32 460.58 165.40 46.76 33.33 31 519.78 43.01 206.37 472.38 178.66 51.08 33.33 32 537.53 47.42 204.29 483.53 192.47 52.60 33.33 33 555.27 52.33 202.08 493.85 206.90 56.51 33.33 34 573.02 57.77 199.72 503.54 221.78 60.40 33.33 35 590.77 63.74 197.19 512.04 237.35 63.86 33.33 36 608.51 70.25 194.47 519.74 253.07 67.06 33.33 37 626.26 77.34 191.55 526.54 269.73 69.11 33.33 38 643.22 85.48 188.38 532.22 286.27 72.94 33.33 39 657.72 94.10 185.09 536.87 302.58 75.97 33.33 40 673.38 105.45 182.03 539.98 316.35 76.73 33.33 41 686.43 116.87 178.42 543.44 327.83 71.90 33.33 42 700.00 131.17 175.11 551.09 339.01 48.70 33.33 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name. intake in. intake out. open 1 LE.txt 1.2 5.5 1 2 LE.txt 1.2 5.5 1 3 LE.txt 1.2 5.5 1 4 LE.txt 1.2 5.5 1 5 LE.txt 1.2 5.5 1 6 LE.txt 1.2 5.5 1 7 LE.txt 1.2 5.5 1 8 LE.txt 1.2 5.5 1 9 LE.txt 1.2 5.5 1 10 LE.txt 1.2 5.5 1 11 LE.txt 1.2 5.5 1 12 LE.txt 1.2 5.5 1 13 LE.txt 1.2 5.5 1 14 LE.txt 1.2 5.5 1 15 LE.txt 1.2 5.5 1 16 LE.txt 1.2 5.5 1 17 LE.txt 1.2 5.5 1 18 LE.txt 1.2 5.5 1 19 LE.txt 1.2 5.5 1 20 LE.txt 1.2 5.5 1 21 LE.txt 1.2 5.5 1 22 LE.txt 1.2 5.5 1 23 LE.txt 1.2 5.5 1 24 LE.txt 1.2 5.5 1 25 LE.txt 1.2 5.5 1 26 LE.txt 1.2 5.5 1 27 LE.txt 1.2 5.5 1 28 LE.txt 1.2 5.5 1 29 LE.txt 1.2 5.5 1 30 LE.txt 1.2 5.5 1 31 LE.txt 1.2 5.5 1 32 LE.txt 1.2 5.5 1 33 LE.txt 1.2 5.5 1 34 LE.txt 1.2 5.5 1 35 LE.txt 1.2 5.5 1 36 LE.txt 1.2 5.5 0 37 LE.txt 1.2 5.5 0 38 LE.txt 1.2 5.5 0 39 LE.txt 1.2 5.5 0 40 LE.txt 1.2 5.5 0 41 LE.txt 1.2 5.5 0 42 LE.txt 1.2 5.5 0 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 0 0 0 0 0 0 0 2 0 0 0 0 0 0 0 3 3 15.5 23.6 67.5 0 0 100 4 0 0 0 0 0 0 0 5 0 0 0 0 0 0 0 6 3 15.5 23.6 67.5 0 0 100 7 0 0 0 0 0 0 0 8 0 0 0 0 0 0 0 9 3 15.5 23.6 67.5 0 0 100 10 0 0 0 0 0 0 0 11 0 0 0 0 0 0 0 12 3 15.5 23.6 67.5 0 0 100 13 0 0 0 0 0 0 0 14 0 0 0 0 0 0 0 15 0 0 0 0 0 0 100 16 0 0 0 0 0 0 0 17 3 15.5 23.6 67.5 0 0 0 18 0 0 0 0 0 0 100 19 0 0 0 0 0 0 0 20 3 15.5 23.6 67.5 0 0 0 21 0 0 0 0 0 0 100 22 0 0 0 0 0 0 0 23 3 15.5 23.6 67.5 0 0 0 24 0 0 0 0 0 0 100 25 0 0 0 0 0 0 0 26 3 15.5 23.6 67.5 0 0 0 27 0 0 0 0 0 0 100 28 0 0 0 0 0 0 0 29 0 0 0 0 0 0 0 30 0 0 0 0 0 0 0 31 2 16.22 70 0 0 0 100 32 2 16.22 70 0 0 0 0 33 0 0 0 0 0 0 0 34 2 16.22 70 0 0 0 100 35 2 16.22 70 0 0 0 0 36 0 0 0 0 0 0 0 37 2 16.22 70 0 0 0 100 38 2 16.22 70 0 0 0 0 39 0 0 0 0 0 0 0 40 2 15 70 0 0 0 100 41 2 8.0 70 0 0 0 0 42 0 0 0 0 0 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 1 42 9 14.59 1.92 2.735 6.72 0. 22.18 1.78 2.375 6.72 0. 33.36 1.64 2.5 5.9 0. 40.32 1.46 2.4 5.8 0. 47.41 1.34 2.23 5.7 0. 59.17 1.27 1.84 3.4 0. 65.23 1.33 1.7 3.2 0. 71.21 1.18 1.6 3.0 0. 81.87 0.89 1.6 1.6 0. ************************************************************* * 5. SKIN TENSION * ************************************************************* Extrados 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. ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 15 upper panels (mm) 15 lower panels (mm) 15 ribs (mm) ************************************************************* * 7. MARKS ************************************************************* 50. 0.5 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 10 * Center of pressure % of chord 50 * Calage % 42 * Risers lenght cm 55 * Line lenght cm 937 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 14 4 1 1 2 1 3 1 4 1 1 3 4 1 1 2 1 3 1 4 2 1 6 4 1 1 2 1 3 2 4 3 1 9 4 1 1 2 1 3 2 4 4 1 12 4 1 1 2 2 3 3 4 5 1 17 4 1 1 2 2 3 3 4 6 1 20 4 1 1 2 2 3 4 4 7 1 23 4 1 1 2 2 3 4 4 8 1 26 4 1 1 2 3 3 5 4 9 1 31 4 1 1 2 3 3 5 4 10 1 32 4 1 1 2 3 3 6 4 11 1 34 4 1 1 2 3 3 6 4 12 1 35 4 1 1 2 3 3 7 4 13 1 37 4 1 1 2 3 3 7 4 14 1 38 4 4 1 1 2 1 3 1 4 1 1 40 4 1 1 2 1 3 1 4 2 2 40 4 1 1 2 1 3 1 4 3 1 41 4 1 1 2 1 3 1 4 4 2 41 14 4 1 1 2 1 3 1 4 1 3 3 4 1 1 2 1 3 1 4 2 3 6 4 1 1 2 1 3 2 4 3 3 9 4 1 1 2 1 3 2 4 4 3 12 4 1 1 2 2 3 3 4 5 3 17 4 1 1 2 2 3 3 4 6 3 20 4 1 1 2 2 3 4 4 7 3 23 4 1 1 2 2 3 4 4 8 3 26 4 1 1 2 3 3 5 4 9 2 31 4 1 1 2 3 3 5 4 10 2 32 4 1 1 2 3 3 6 4 11 2 34 4 1 1 2 3 3 6 4 12 2 35 4 1 1 2 3 3 7 4 13 2 37 4 1 1 2 3 3 7 4 14 2 38 *************************************************** * 10. BRAKES *************************************************** 330 12 4 1 1 2 1 3 1 4 1 6 6 4 1 1 2 1 3 1 4 2 6 9 4 1 1 2 1 3 2 4 3 6 12 4 1 1 2 1 3 2 4 4 6 15 4 1 1 2 2 3 3 4 5 6 18 4 1 1 2 2 3 3 4 6 6 21 4 1 1 2 2 3 4 4 7 6 24 4 1 1 2 2 3 4 4 8 6 27 4 1 1 2 3 3 5 4 9 6 31 4 1 1 2 3 3 5 4 10 6 34 4 1 1 2 3 3 6 4 11 6 37 4 1 1 2 3 3 6 4 12 6 40 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 350 180 3 100 4 200 80 ***************************************************