************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file (leparagliding 3.18) * ************************************************************** * Date: 2020-11-22 > 2022-04-03 * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "BHL4-31" * Drawing scale 1.0 * Wing scale 1.136 * Number of cells 34 * Number of ribs 35 * Alpha wingtip, parameter, (alpha center) 9.0 0 0.0 * Paraglider type and parameter "ss" 1 * Rib geometric parameters *Rib x-rib y-LE y-TE xp z beta RP Washin 1 17.29 0.09 280.50 17.28 0.23 1.51 33.33 0.00 2 51.80 0.78 280.16 51.74 2.08 4.67 33.33 0.00 3 86.18 2.18 279.50 85.92 5.76 7.68 33.33 0.00 4 120.37 4.26 278.49 119.67 11.22 10.70 33.33 0.00 5 154.31 7.04 277.16 152.84 18.40 13.72 33.33 0.00 6 187.93 10.53 275.49 185.21 27.46 17.64 33.33 0.00 7 221.17 14.72 273.48 216.48 38.71 21.78 33.33 0.00 8 253.96 19.63 271.12 246.46 51.98 25.93 33.33 0.00 9 286.22 25.60 268.42 274.95 67.09 29.86 33.33 0.25 10 317.83 33.00 265.38 301.78 83.79 33.80 33.33 1.00 11 348.69 41.78 261.98 326.62 102.08 39.23 33.33 2.00 12 378.70 51.90 258.24 348.91 122.15 44.71 33.33 3.00 13 407.75 63.30 254.11 368.52 143.57 50.20 33.33 4.00 14 435.65 77.00 249.17 385.37 165.80 55.46 33.33 5.00 15 462.13 94.32 243.36 399.31 188.30 61.15 33.33 6.00 16 486.96 114.60 236.81 410.21 210.59 66.80 33.33 7.00 17 509.95 137.12 229.68 418.36 232.09 71.81 33.33 8.00 18 531.00 161.16 222.12 424.75 255.10 76.41 33.33 9.00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open, disp, rrw 1 bhl-5p.txt 2.244 10.0 1 0 1 1 2 bhl-5p.txt 2.244 10.0 1 0 1 1 3 bhl-5p.txt 2.244 10.0 1 0 1 1 4 bhl-5p.txt 2.244 10.0 1 0 1 1 5 bhl-5p.txt 2.244 10.0 1 0 1 1 6 bhl-5p.txt 2.244 10.0 1 0 1 1 7 bhl-5p.txt 2.244 10.0 1 0 1 1 8 bhl-5p.txt 2.244 10.0 1 0 1 1 9 bhl-5p.txt 2.244 10.0 1 0 1 1 10 bhl-5p.txt 2.244 10.0 1 0 1 1 11 bhl-5p.txt 2.244 10.0 1 0 1 1 12 bhl-5p.txt 2.244 10.0 1 0 1 1 13 bhl-4p.txt 2.244 10.0 1 0 1 1 14 bhl-4p.txt 2.244 10.0 1 0 1 1 15 bhl-4p.txt 2.244 10.0 1 0 1 1 16 bhl-tube.txt 2.244 10.0 1 0 1 0 17 bhl-tube.txt 2.244 10.0 1 0 1 0 28 bhl-tube.txt 2.244 10.0 1 0 1 0 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 5 10. 30.35 49.29 67.54 85.00 100 2 5 10. 30.35 49.29 67.54 85.00 100 3 5 10. 30.35 49.29 67.54 85.00 100 4 5 10. 30.35 49.29 67.54 85.00 100 5 5 10. 30.35 49.29 67.54 85.00 100 6 5 10. 30.35 49.29 67.54 85.00 100 7 5 10. 30.35 49.29 67.54 85.00 100 8 5 10. 30.35 49.29 67.54 85.00 100 9 5 10. 30.35 49.29 67.54 85.00 100 10 5 10. 30.35 49.29 67.54 85.00 100 11 5 10. 30.35 49.29 67.54 85.00 100 12 5 10. 30.35 49.29 67.54 85.00 100 13 5 10. 30.35 49.29 67.54 85.00 100 14 4 10. 30.35 51.32 75.28 0.0 100 15 4 10. 30.35 51.32 75.28 0.0 100 16 4 10. 30.35 51.32 75.28 0 100 17 1 10. 0.0 0.0 0.0 0 100 18 4 5. 33 66 95 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 17 17 6 1 5.6772 1.2020 2.55 2.55 0. 0. 0. 1 19.1340 3.1953 5.17 5.17 0. 0. 0. 1 34.9116 3.7191 4.30 4.30 0. 0. 0. 1 48.5396 3.2010 3.38 3.38 0. 0. 0. 1 60.3734 2.6921 2.45 2.45 0. 0. 0. 1 71.3037 2.2690 1.75 1.75 0. 0. 0. ************************************************************* * 5. SKIN TENSION * ************************************************************* Extrados Intrados 0. 0. 0. 0. 7.5 1.3 10. 1.33 15. 2.8 20. 2.8 80. 2.8 80. 2.8 90. 1.33 90. 1.33 100. 0.0 100. 0. 0.0001 1000 1.0 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 15 25 25 upper panels (mm) 15 25 25 lower panels (mm) 15 ribs (mm) 15 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25 0.03 0.135 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 7.0 * Center of pressure % of chord 45 * Calage % 41 * Risers lenght cm 47 * Line lenght cm 636 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 4 16 4 1 1 2 1 3 1 4 1 1 1 4 1 1 2 1 3 1 4 2 1 2 4 1 1 2 1 3 2 4 3 1 3 4 1 1 2 1 3 2 4 4 1 4 4 1 1 2 2 3 3 4 5 1 5 4 1 1 2 2 3 3 4 6 1 6 4 1 1 2 2 3 3 4 7 1 7 4 1 1 2 2 3 4 4 8 1 8 4 1 1 2 2 3 4 4 9 1 9 4 1 1 2 2 3 4 4 10 1 10 4 1 1 2 3 3 5 4 11 1 11 4 1 1 2 3 3 5 4 12 1 12 4 1 1 2 3 3 5 4 13 1 13 4 1 1 2 3 3 6 4 14 1 14 4 1 1 2 3 3 6 4 15 1 15 4 1 1 2 3 3 6 4 16 1 16 16 4 1 1 2 1 3 1 4 1 2 1 4 1 1 2 1 3 1 4 2 2 2 4 1 1 2 1 3 2 4 3 2 3 4 1 1 2 1 3 2 4 4 2 4 4 1 1 2 2 3 3 4 5 2 5 4 1 1 2 2 3 3 4 6 2 6 4 1 1 2 2 3 3 4 7 2 7 4 1 1 2 2 3 4 4 8 2 8 4 1 1 2 2 3 4 4 9 2 9 4 1 1 2 2 3 4 4 10 2 10 4 1 1 2 3 3 5 4 11 2 11 4 1 1 2 3 3 5 4 12 2 12 4 1 1 2 3 3 5 4 13 2 13 4 1 1 2 3 3 6 4 14 2 14 4 1 1 2 3 3 6 4 15 2 15 4 1 1 2 3 3 6 4 16 2 16 20 4 1 1 2 1 3 1 4 1 3 1 4 1 1 2 1 3 1 4 2 3 2 4 1 1 2 1 3 2 4 3 3 3 4 1 1 2 1 3 2 4 4 3 4 4 1 1 2 2 3 3 4 5 3 5 4 1 1 2 2 3 3 4 6 3 6 4 1 1 2 2 3 3 4 7 3 7 4 1 1 2 2 3 4 4 8 3 8 4 1 1 2 2 3 4 4 9 3 9 4 1 1 2 2 3 4 4 10 3 10 4 1 1 2 3 3 5 4 11 3 11 4 1 1 2 3 3 5 4 12 3 12 4 1 1 2 3 3 5 4 13 3 13 4 1 1 2 3 3 6 4 14 3 14 4 1 1 2 3 3 6 4 15 3 15 4 1 1 2 3 3 6 4 16 3 16 3 1 1 2 4 3 7 0 0 1 18 3 1 1 2 4 3 8 0 0 2 18 3 1 1 2 4 3 9 0 0 3 18 3 1 1 2 4 3 10 0 0 4 18 29 4 1 1 2 1 3 1 4 1 4 1 4 1 1 2 1 3 1 4 2 5 1 4 1 1 2 1 3 1 4 3 4 2 4 1 1 2 1 3 1 4 4 5 2 4 1 1 2 1 3 2 4 5 4 3 4 1 1 2 1 3 2 4 6 5 3 4 1 1 2 1 3 2 4 7 4 4 4 1 1 2 1 3 2 4 8 5 4 4 1 1 2 2 3 3 4 9 4 5 4 1 1 2 2 3 3 4 10 5 5 4 1 1 2 2 3 3 4 11 4 6 4 1 1 2 2 3 3 4 12 5 6 4 1 1 2 2 3 3 4 13 4 7 4 1 1 2 2 3 3 4 14 5 7 4 1 1 2 2 3 4 4 15 5 8 4 1 1 2 2 3 4 4 16 4 8 4 1 1 2 2 3 4 4 17 5 9 4 1 1 2 2 3 4 4 18 4 9 4 1 1 2 2 3 4 4 19 5 10 4 1 1 2 2 3 4 4 20 5 10 4 1 1 2 3 3 5 4 21 4 11 4 1 1 2 3 3 5 4 22 5 11 4 1 1 2 3 3 5 4 23 4 12 4 1 1 2 3 3 5 4 24 5 12 4 1 1 2 3 3 5 4 25 4 13 4 1 1 2 3 3 5 4 26 5 13 4 1 1 2 3 3 6 4 27 4 14 4 1 1 2 3 3 6 4 28 4 15 4 1 1 2 3 3 6 4 29 4 16 *************************************************** * 10. BRAKES *************************************************** 230 9 3 1 1 2 1 3 1 0 0 6 1 3 1 1 2 1 3 2 0 0 6 3 3 1 1 2 1 3 3 0 0 6 5 3 1 1 2 2 3 4 0 0 6 7 3 1 1 2 2 3 5 0 0 6 9 3 1 1 2 2 3 6 0 0 6 11 3 1 1 2 3 3 7 0 0 6 13 3 1 1 2 3 3 8 0 0 6 15 3 1 1 2 3 3 9 0 0 6 17 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 150 4 250 100 3 160 4 250 100 *************************************************** * 12. H V and VH ribs *************************************************** 5 80 150 1 1 0 1 1 1 2.5 0 0 0 2 1 4 1 5 1 2.5 0 0 0 3 1 7 1 8 1 2.5 0 0 0 4 1 10 1 11 1 2.5 0 0 0 5 1 13 1 14 1 2.5 0 0 0 ***************************************************** * 15. Extrados colors ***************************************************** 3 1 1 1 40.1 0. 2 1 1 20.15 0. 3 1 1 0.0 0. ***************************************************** * 16. Intrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 17. Aditional rib points ***************************************************** 0 ***************************************************** * 18. Elastic lines corrections ***************************************************** 180 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 3.0 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) ******************************************************* 1 2 1 1 15 5.5 10. 1.5 2.0 5. 10. 2.2 2.0 0.0 9.35 6.3 9.35 2 16 17 5. 9. 2.5 2.0 5. 12 3. 2.0 0.0 9.35 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 1 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 1 2 1 3 1 4 1 5 1 6 1 7 1 8 1 9 1 10 1 11 1 12 1 13 1 14 1 15 1 16 1 17 1 18 1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 4 10. 30.35 49.29 76.27 0 0 -3.0 3 5.0 10 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 18 upper 0 1 lower 0 1 * Print parameters Inter3D 1 1 10 1 Ovali3D 1 1 14 0 tesse3D 0 1 14 0 exteDXF 0 1 14 0 exteSTL 0 1 14 0 ******************************************************* * 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 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 18, 14 points, type "1" 1 1 18 14 1 1 0. 0.03 0. 0. 2 5. 0.4 10. 0.625 3 10.0 1.0 20. 1.25 4 15. 1.94 30. 1.875 5 17.5 2.93 35 2.1875 6 20. 3.32 40. 2.5 7 25. 3.5 65. 2.5 8 50. 3.5 70. 2.4 9 55. 3.33 75. 2.3 10 65. 2.77 80. 2.0 11 70. 2.35 85. 1.5 12 90. 0.67 90. 0.9 13 95. 0.19 95. 0.3 14 100. 0.0 100. 0.03 ******************************************************* * 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 1.0 rib_1y 1.8 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0