************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file versions 3.18 and 3.26ed (test versions) * ************************************************************** * Version 2022-09-18 uodate to 2025-07-29 * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "LABORATORI D'ENVOL" * Wing name "HEGALA v2" * Drawing scale 1. * Wing scale 1 * Number of cells 28 * Number of ribs 29 * Alpha max and parameter 7.0 0 * Paraglider type and parameter "ds" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 0.00000000 0.00000000 212.10000000 0.00000000 0.00000000 0.00 0.00 0.00 2 30.82000000 0.09000000 212.10000000 30.81331042 0.64210686 3.08 0.00 0.00 3 61.57000000 0.79000000 211.98621568 61.43436017 3.31064799 6.84 0.00 0.00 4 92.14000000 2.18000000 211.78530258 91.64444707 7.94105291 10.58 0.00 0.00 5 122.45000000 4.28000000 211.48670703 121.24269386 14.47873220 14.30 0.00 0.00 6 152.42000000 7.09000000 211.09332511 150.02899393 22.82130842 17.97 0.00 0.00 7 181.96000000 10.63000000 210.60901959 177.81660046 32.82252016 21.58 0.00 0.00 8 210.98000000 14.92000000 210.03858458 204.44061235 44.33895941 25.14 0.00 0.00 9 239.39000000 19.98000000 209.38776137 229.76817354 57.19942768 28.71 0.00 0.00 10 267.10000000 25.88000000 208.66325505 253.62000684 71.27941519 33.61 0.00 0.00 11 293.88000000 34.24000000 207.87708560 275.04752583 87.29149282 40.46 0.00 0.5 12 319.44000000 46.07000000 207.04607610 293.31654720 105.13227078 48.91 0.00 1.8 13 343.40000000 61.89719877 206.46815741 307.41714698 124.43540228 58.77 0.00 3.5 14 365.41000000 87.85725464 206.19378519 317.01744862 144.24131828 69.59 0.00 5 15 375.2440 124.34976184 206.19378519 319.1556 153.8259 77.07 0.00 7 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open , disp, rrw, minirib 1 profil.txt 1.1 4.25 1 0 1 15 2 profil.txt 1.1 4.25 1 0 1 15 3 profil.txt 1.1 4.25 1 0 1 15 4 profil.txt 1.1 4.25 1 0 1 15 5 profil.txt 1.1 4.25 1 0 1 15 6 profil.txt 1.1 4.25 1 0 1 15 7 profil.txt 1.1 4.25 1 0 1 15 8 profil.txt 1.1 4.25 1 0 1 15 9 profil.txt 1.1 4.25 1 0 1 15 10 profil.txt 1.1 4.25 1 0 1 15 11 profil.txt 1.1 4.25 1 0 1 15 12 profil.txt 0 0 0 0 1 15 13 profil.txt 0 0 0 0 1 15 14 profil.txt 0 0 0 0 1 15 15 profil.txt 0 0 0 0 1 15 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 0 9.35 34.95 69.63 0 0 0 2 4 9.35 34.95 69.63 98.11 0 98.11 3 0 9.35 34.95 69.63 0 0 0 4 4 9.35 34.95 69.63 98.09 0 98.09 5 0 9.35 34.95 69.63 0 0 0 6 4 9.35 34.95 69.63 98.04 0 98.04 7 0 9.35 34.95 69.63 0 0 0 8 4 9.35 34.95 69.63 97.94 0 97.94 9 0 9.35 34.95 69.63 0 0 0 10 4 9.35 34.95 69.63 97.81 0 97.81 11 0 9.35 34.95 69.63 0 0 0 12 4 9.35 34.95 69.63 97.51 0 97.51 13 0 9.35 34.95 69.63 0 0 0 14 3 12 60 96.62 0 0 96.62 15 0 0 0 0 0 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 14 1 1 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 2 2 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 3 3 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 4 4 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 5 5 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 6 6 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 7 7 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 8 8 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 9 9 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 10 10 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 11 11 9 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 36.2 0.4 3.06 7.57 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 68.77 -0.496 1.95 4.02 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 12 12 7 1 15.6 -3.73 1.06 2.03 0. 0. 0. 0. 1 21.7 1.25 3.09 7.71 0. 0. 0. 0. 1 28.2 -4.9 1.13 2.04 0. 0. 0. 0. 1 45.5 -4.37 1.41 2.49 0. 0. 0. 0. 1 52.42 -0.25 3.07 6.08 0. 0. 0. 0. 1 59.78 -3.06 1.41 2.5 0. 0. 0. 0. 1 79.18 -0.45 1.5 2.3 0. 0. 0. 0. 13 13 8 1 15.6 -3.17 1.06 1.73 0 0 0 0 1 21.7 1.06 3.09 6.55 0 0 0 0 1 28.2 -4.17 1.13 1.73 0 0 0 0 1 36.2 0.34 3.06 6.43 0 0 0 0 1 45.5 -3.71 1.41 2.12 0 0 0 0 1 52.42 -0.21 3.07 5.17 0 0 0 0 1 59.78 -2.60 1.41 2.13 0 0 0 0 1 79.18 -0.38 1.5 1.96 0 0 0 0 14 14 7 1 15.6 -2.61 1.06 1.42 0 0 0 0 1 21.7 0.88 3.09 5.40 0 0 0 0 1 28.2 -3.43 1.13 1.43 0 0 0 0 1 36.2 0.28 3.06 5.3 0. 0. 0. 0. 1 45.5 -3.06 1.41 1.74 0 0 0 0 1 52.42 -0.18 3.07 4.26 0 0 0 0 1 79.18 -0.32 1.5 1.61 0 0 0 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. 0.0114 1000 1.0 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 10 10 20 upper panels (mm) 10 10 20 lower panels (mm) 10 ribs (mm) 10 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.05 0.0 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 5 * Center of pressure % of chord 41.6 * Calage % 31 * Risers lenght cm 47 * Line lenght cm 430 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 3 6 3 1 1 2 1 3 1 0 0 1 2 - 1 2 3 3 1 1 2 1 3 2 0 0 1 4 - 1 2 3 3 1 1 2 1 3 3 0 0 1 6 - 1 2 3 3 1 1 2 2 3 4 0 0 1 8 - 1 2 3 3 1 1 2 2 3 5 0 0 1 10 - 1 2 3 3 1 1 2 2 3 6 0 0 1 12 - 1 2 3 8 3 1 1 2 1 3 1 0 0 2 2 - 1 2 3 3 1 1 2 1 3 2 0 0 2 4 - 1 2 3 3 1 1 2 1 3 3 0 0 2 6 - 1 2 3 3 1 1 2 2 3 4 0 0 2 8 - 1 2 3 3 1 1 2 2 3 5 0 0 2 10 - 1 2 3 3 1 1 2 2 3 6 0 0 2 12 - 1 2 3 3 1 1 2 3 3 7 0 0 1 14 - 1 2 3 3 1 1 2 3 3 8 0 0 2 14 - 1 2 3 6 3 1 1 2 1 3 1 0 0 3 2 - 1 2 3 3 1 1 2 1 3 2 0 0 3 4 - 1 2 3 3 1 1 2 1 3 3 0 0 3 6 - 1 2 3 3 1 1 2 2 3 4 0 0 3 8 - 1 2 3 3 1 1 2 2 3 5 0 0 3 10 - 1 2 3 3 1 1 2 2 3 6 0 0 3 12 - 1 2 3 *************************************************** * 10. BRAKES *************************************************** 150 7 3 1 1 2 1 3 1 0 0 6 2 - 6 2 3 3 1 1 2 1 3 2 0 0 6 4 - 6 2 3 3 1 1 2 2 3 3 0 0 6 6 - 6 2 3 3 1 1 2 2 3 4 0 0 6 8 - 6 2 3 3 1 1 2 3 3 5 0 0 6 10 - 6 2 3 3 1 1 2 3 3 6 0 0 6 12 - 6 2 3 3 1 1 2 3 3 7 0 0 6 14 - 6 2 3 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 160 4 150 100 3 150 4 200 70 *************************************************** * 12. H V and VH ribs *************************************************** 21 80 150 1 11 1 1 2 1 1.5 0.0 0 0 2 11 1 2 2 2 1.5 0.0 0 0 3 11 1 3 2 3 1.5 0.0 0 0 4 13 2 1 1 1 1.5 6.0 0 0 5 13 4 1 1 1 1.5 6.0 0 0 6 13 6 1 1 1 1.5 6.0 0 0 7 13 8 1 1 1 1.5 6.0 0 0 8 13 10 1 1 1 1.5 6.0 0 0 9 13 12 1 1 1 1.5 6.0 0 0 10 13 2 2 1 1 1.5 6.0 0 0 11 13 4 2 1 1 1.5 6.0 0 0 12 13 6 2 1 1 1.5 6.0 0 0 13 13 8 2 1 1 1.5 6.0 0 0 14 13 10 2 1 1 1.5 6.0 0 0 15 13 12 2 1 1 1.5 6.0 0 0 16 13 2 3 1 1 1.5 6.0 0 0 17 13 4 3 1 1 1.5 6.0 0 0 18 13 6 3 1 1 1.5 6.0 0 0 19 13 8 3 1 1 1.5 6.0 0 0 20 13 10 3 1 1 1.5 6.0 0 0 21 13 12 3 1 1 1.5 6.0 0 0 ***************************************************** * 15. Extrados colors ***************************************************** 15 1 1 1 94 0. 2 1 1 94 0. 3 1 1 94 0. 4 1 1 94 0. 5 1 1 94 0. 6 1 1 94 0. 7 1 1 94 0. 8 1 1 94 0. 9 1 1 94 0. 10 1 1 94 0. 11 1 1 94 0. 12 1 1 94 0. 13 1 1 94 0. 14 1 1 94 0. 15 1 1 0 0. ***************************************************** * 16. Intrados colors ***************************************************** 15 1 1 1 78 0. 2 1 1 85 0. 3 1 1 85 0. 4 1 1 85 0. 5 1 1 85 0. 6 1 1 85 0. 7 1 1 85 0. 8 1 1 85 0. 9 1 1 85 0. 10 1 1 85 0. 11 1 1 85 0. 12 1 1 85 0. 13 1 1 85 0. 14 1 1 85 0. 15 1 1 0 0. ***************************************************** * 17. Aditional rib points ***************************************************** 1 100 10 ***************************************************** * 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 1.5 0 2 0.05 1.0 typepoint2 1 1.5 0 2 0.05 1.2 typepoint3 1 1.5 0 2 0.05 1.2 typevent 1 10. 0.0 1 6.0 3.0 typetab 1 10. 0.0 3 1.8 5.0 typejonc 1 10. 0.0 2 0.05 1.2 typeref 1 5. 1. 1 2.0 0.0 type8 1 0.25 5 2 0.05 5 type9 1 0.25 5 2 0.05 5 type10 1 0.25 5 2 0.05 5 ******************************************************* * 21. JONCS DEFINITION (NYLON RODS) ******************************************************* 1 1 1 1 14 14 20 0.8 2.0 2.62 8.62 0.8 2.0 3 13 3.0 10.0 ******************************************************* * 22. NOSE MYLARS DEFINITION ******************************************************* 0 ******************************************************* * 23. TAB REINFORCEMENTS ******************************************************* 0 ******************************************************* * 24. GENERAL 2D DXF OPTIONS ******************************************************* 1 A_lines_color 1 rouge B_lines_color 30 orange C_lines_color 3 green D_lines_color 4 cyan E_lines_color 6 magenta F_lines_color 6 magenta ******************************************************* * 25. GENERAL 3D DXF OPTIONS ******************************************************* 1 A_lines_color 1 rouge B_lines_color 30 orange C_lines_color 3 green D_lines_color 4 cyan E_lines_color 6 magenta F_lines_color 6 magenta Extrados 1 5 bleu Vents 0 1 rouge Intrados 1 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 -2 2 -3 3 -2 4 -3 5 -2 6 -3 7 -2 8 -3 9 -2 10 -3 11 -2 12 -1 13 -1 14 -1 15 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 3 9.35 34.95 69.63 0 0 0 -5 20 4 20 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 15 upper 0 1 lower 0 1 * Print parameters Inter3D 0 1 10 1 Ovali3D 0 1 14 0 tesse3D 1 1 15 1 exteDXF 1 1 15 1 exteSTL 1 1 15 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 0.85 14 0.7 15 0.1 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 2 * Skin tension group number "1" from rib 1 to 11, 6 points, type "1" 1 1 11 6 1 1 0.0 0.0 0.0 0.0 2 3.38 0.0 24 2.0 3 7.0 0.1 50 2.5 4 25 2.5 84 2.0 5 76 2.2 95 0.7 6 100 0.0 100 0.0 * Skin tension group number "2" from rib 12 to 15, 6 points, type "1" 1 12 15 6 1 1 0.0 0.0 0.0 0.0 2 3.38 0.0 24 2.0 3 7.0 0.1 50 2.5 4 25 2.5 84 2.0 5 76 2.2 95 0.7 6 100 0.0 100 0.0 ******************************************************* * 32. PARAMETERS FOR PARTS SEPARATION ******************************************************* 1 panel_x 1.2 panel_x_min 1.0 panel_y 0.8 rib_x 1.0 rib_y 1.8 parameter6 1.0 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0 ******************************************************* * 33. DETAILED RISERS ******************************************************* 1 1 A 50.0 cm B 50.0 cm C 80.0 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 ******************************************************* 0 ******************************************************* * 36. CREATE FILES FOR XFLR5 ANALYSIS ******************************************************* 0 ******************************************************* * 37. SOME SPECIAL PARAMETERS ******************************************************* 0