************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file * ************************************************************** * ************************************************************** * 1. GEOMETRY * ************************************************************** * Wing name gnuLAB2 * Number of cells 29 * Number of ribs 30 * Alpha max 4.5 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP 1 20 0 286.52 20 0.3 1.653 33.33 2 60 0.97 286.04 59.94 2.54 4.786 33.33 3 100 2.78 285.08 99.68 7.09 8.282 33.33 4 140 5.55 283.61 139.06 14.06 11.581 33.33 5 180 9.32 281.61 178.03 23.1 15.183 33.33 6 220 14.17 279.06 216.32 34.87 19.036 33.33 7 260 20.19 275.90 253.66 49.77 22.906 33.33 8 300 27.5 272.05 289.81 66.33 26.598 33.33 9 340 37.02 267.42 324.65 85.98 32.117 33.33 10 380 49.53 261.85 357.49 108.82 37.604 33.33 11 420 64.87 255.1 387.27 134.39 43.775 33.33 12 457.2 83.01 247.4 413.08 161.20 49.639 33.33 13 489.2 103.46 239.17 431.85 187.12 59.571 33.33 14 517.2 127.8 230.68 443.16 212.74 74.465 33.33 15 542.2 158.04 223.3 442.51 237.73 90.000 33.33 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open 1 gnulab2.txt 1.2 5.5 1 2 gnulab2.txt 1.2 5.5 1 3 gnulab2.txt 1.2 5.5 1 4 gnulab2.txt 1.2 5.5 1 5 gnulab2.txt 1.2 5.5 1 6 gnulab2.txt 1.2 5.5 1 7 gnulab2.txt 1.2 5.5 1 8 gnulab2.txt 1.2 5.5 1 9 gnulab2.txt 1.2 5.5 1 10 gnulab2.txt 1.2 5.5 1 11 gnulab2.txt 1.2 5.5 1 12 gnulab2.txt 1.2 5.5 1 13 gnulab2.txt 1.2 5.5 0 14 gnulab2.txt 1.2 5.5 0 15 airplan.txt 1.2 5.5 0 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 4 8.5 27.5 53 77 0 0 2 4 8.5 27.5 53 77 0 100 3 4 8.5 27.5 53 77 0 100 4 4 8.5 27.5 53 77 0 100 5 4 8.5 27.5 53 77 0 100 6 4 8.5 27.5 53 77 0 100 7 4 8.5 27.5 53 77 0 100 8 4 8.5 27.5 53 77 0 100 9 4 8.5 27.5 53 77 0 100 10 4 8.5 27.5 53 77 0 100 11 4 8.5 27.5 53 77 0 100 12 4 8.5 27.5 53 77 0 100 13 3 8.5 40.0 75 0 0 100 14 3 8.5 40.0 75 0 0 100 15 3 8.5 40.0 75 0 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 2 1 12 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. 13 15 3 23.5 1.92 6.5 6.5 0. 55.0 1.92 4.3 4.3 0. 81. 1.1 1.7 1.7 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 7 * Center of pressure % of chord 25 * Calage % 20 * Risers lenght cm 55 * Line lenght cm 650 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 4 16 3 1 1 2 1 3 1 0 0 1 1 3 1 1 2 1 3 2 0 0 1 2 3 1 1 2 1 3 3 0 0 1 3 3 1 1 2 2 3 4 0 0 1 4 3 1 1 2 2 3 5 0 0 1 5 3 1 1 2 2 3 6 0 0 1 6 3 1 1 2 3 3 7 0 0 1 7 3 1 1 2 3 3 8 0 0 1 8 3 1 1 2 3 3 9 0 0 1 9 3 1 1 2 4 3 10 0 0 1 10 3 1 1 2 4 3 11 0 0 1 11 3 1 1 2 4 3 12 0 0 1 12 3 1 1 2 5 3 13 0 0 1 13 3 1 1 2 5 3 14 0 0 1 14 3 1 1 2 5 3 15 0 0 2 13 3 1 1 2 5 3 16 0 0 2 14 16 3 1 1 2 1 3 1 0 0 2 1 3 1 1 2 1 3 2 0 0 2 2 3 1 1 2 1 3 3 0 0 2 3 3 1 1 2 2 3 4 0 0 2 4 3 1 1 2 2 3 5 0 0 2 5 3 1 1 2 2 3 6 0 0 2 6 3 1 1 2 3 3 7 0 0 2 7 3 1 1 2 3 3 8 0 0 2 8 3 1 1 2 3 3 9 0 0 2 9 3 1 1 2 4 3 10 0 0 2 10 3 1 1 2 4 3 11 0 0 2 11 3 1 1 2 4 3 12 0 0 2 12 3 1 1 2 5 3 13 0 0 1 15 3 1 1 2 5 3 14 0 0 2 15 3 1 1 2 5 3 15 0 0 3 15 3 1 1 2 5 3 16 0 0 3 14 12 3 1 1 2 1 3 1 0 0 3 1 3 1 1 2 1 3 2 0 0 3 2 3 1 1 2 1 3 3 0 0 3 3 3 1 1 2 2 3 4 0 0 3 4 3 1 1 2 2 3 5 0 0 3 5 3 1 1 2 2 3 6 0 0 3 6 3 1 1 2 3 3 7 0 0 3 7 3 1 1 2 3 3 8 0 0 3 8 3 1 1 2 3 3 9 0 0 3 9 3 1 1 2 4 3 10 0 0 3 10 3 1 1 2 4 3 11 0 0 3 11 3 1 1 2 4 3 12 0 0 3 12 13 3 1 1 2 1 3 1 0 0 4 1 3 1 1 2 1 3 2 0 0 4 2 3 1 1 2 1 3 3 0 0 4 3 3 1 1 2 2 3 4 0 0 4 4 3 1 1 2 2 3 5 0 0 4 5 3 1 1 2 2 3 6 0 0 4 6 3 1 1 2 3 3 7 0 0 4 7 3 1 1 2 3 3 8 0 0 4 8 3 1 1 2 3 3 9 0 0 4 9 3 1 1 2 4 3 10 0 0 4 10 3 1 1 2 4 3 11 0 0 4 11 3 1 1 2 4 3 12 0 0 4 12 3 1 1 2 4 3 13 0 0 3 13 *************************************************** * 10. BRAKES *************************************************** 250 14 4 1 1 2 1 3 1 4 1 6 2 4 1 1 2 1 3 1 4 2 6 3 4 1 1 2 1 3 2 4 3 6 4 4 1 1 2 1 3 2 4 4 6 5 4 1 1 2 2 3 3 4 5 6 6 4 1 1 2 2 3 3 4 6 6 7 4 1 1 2 2 3 4 4 7 6 8 4 1 1 2 2 3 4 4 8 6 9 4 1 1 2 3 3 5 4 9 6 10 4 1 1 2 3 3 5 4 10 6 11 4 1 1 2 3 3 5 4 11 6 12 4 1 1 2 3 3 6 4 12 6 13 4 1 1 2 3 3 6 4 13 6 14 4 1 1 2 3 3 6 4 14 6 15 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 350 180 3 100 4 200 80 ***************************************************