************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file (leparagliding 3.17+) * ************************************************************** * File update 2022-02-08 ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "LABORATORI D'ENVOL" * Wing name "BHL7-10" * Drawing scale 1. * Wing scale 0.660916031 * Number of cells 33 * Number of ribs 34 * Alpha max and parameter 6.5 1 * Paraglider type and parameter "ss" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 18.47 .09 268.04 18.46 .24 1.53 33.33 .00 0.22 50.0 2 55.32 .83 267.63 55.26 2.11 4.31 33.33 .00 0.61 50.0 3 92.01 2.31 266.81 91.76 5.83 7.23 33.33 .00 1.02 50.0 4 128.47 4.52 265.58 127.80 11.36 10.15 33.33 .00 1.43 50.0 5 164.61 7.48 263.94 163.19 18.62 13.00 33.33 .00 1.82 50.0 6 200.35 11.21 261.89 197.71 27.87 17.10 33.33 .00 2.38 50.0 7 235.61 15.70 259.42 231.02 39.40 21.21 33.33 .00 2.93 50.0 8 270.31 20.99 256.53 262.94 53.01 25.05 33.33 .00 3.43 50.0 9 304.35 27.17 253.23 293.25 68.48 28.90 33.33 .00 3.92 50.0 10 337.58 35.25 249.50 321.77 85.54 32.74 33.33 .00 4.39 50.0 11 369.82 45.51 245.36 348.28 103.86 36.59 33.33 .00 4.84 50.0 12 400.89 57.85 240.70 372.58 123.21 41.19 33.33 .00 5.34 50.0 13 430.61 72.15 235.40 393.83 143.97 47.35 33.33 .00 5.97 50.0 14 458.81 88.29 229.50 411.86 165.64 53.11 33.33 .00 6.49 50.0 15 485.33 106.21 223.07 426.73 187.58 59.33 33.33 .00 6.99 50.0 16 510.02 125.97 216.19 436.26 210.27 75.16 33.33 .00 7.86 50.0 17 532.69 147.88 208.94 439.31 234.36 89.34 33.33 .00 8.13 50.0 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open, disp, rrw 1 bhlnm-4p.txt 2.244 10.0 1 0 1 1 2 bhlnm-4p.txt 2.244 10.0 1 0 1 1 3 bhlnm-4p.txt 2.244 10.0 1 0 1 1 4 bhlnm-4p.txt 2.244 10.0 1 0 1 1 5 bhlnm-4p.txt 2.244 10.0 1 0 1 1 6 bhlnm-4p.txt 2.244 10.0 1 0 1 1 7 bhlnm-4p.txt 2.244 10.0 1 0 1 1 8 bhlnm-4p.txt 2.244 10.0 1 0 1 1 9 bhlnm-4p.txt 2.244 10.0 1 0 1 1 10 bhlnm-4p.txt 2.244 10.0 1 0 1 1 11 bhlnm-4p.txt 2.244 10.0 1 0 1 1 12 bhlnm-4p.txt 2.244 10.0 1 0 1 1 13 bhlnm-4p.txt 2.244 10.0 1 0 1 1 14 bhlnm-4p.txt 2.244 10.0 1 0 1 1 15 gnuPSFtube.txt 2.244 10.0 1 0 1 0 16 gnuPSFtube.txt 2.244 10.0 1 0 1 0 17 gnuPSFtube.txt 2.244 10.0 1 0 1 0 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 4 10. 30.35 51.32 75.28 0 0 2 4 10. 30.35 51.32 75.28 0 100 3 4 10. 30.35 51.32 75.28 0 100 4 4 10. 30.35 51.32 75.28 0 100 5 4 10. 30.35 51.32 75.28 0 100 6 4 10. 30.35 51.32 75.28 0 100 7 4 10. 30.35 51.32 75.28 0 100 8 4 10. 30.35 51.32 75.28 0 100 9 4 10. 30.35 51.32 75.28 0 100 10 4 10. 30.35 51.32 75.28 0 100 11 4 10. 30.35 51.32 75.28 0 100 12 4 10. 30.35 51.32 75.28 0 100 13 4 10. 30.35 51.32 75.28 0 100 14 4 10. 30.35 51.32 75.28 0 100 15 3 10. 41.12 78.00 0.0 0 100 16 0 10. 41.12 78.00 0.0 0 100 17 4 2.244 33 66 95 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 16 16 5 1 20.1 3.0 4.0 5.1 0. 0. 0. 1 33.7 3.4 4.0 5.1 0. 0. 0. 1 50.3 3.2 4.0 4.0 0. 0. 0. 1 62.4 2.7 3.2 3.2 0. 0. 0. 1 72.4 2.3 1.8 1.8 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 * ************************************************************* 15 25 25 upper panels (mm) 15 25 25 lower panels (mm) 15 ribs (mm) 15 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.5 0.12 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 7.0 * Center of pressure % of chord 45 * Calage % 42 * Risers lenght cm 47 * Line lenght cm 645 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 3 15 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 4 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 3 3 5 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 6 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 19 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 4 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 3 3 5 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 6 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 3 1 1 2 4 3 7 0 0 1 17 3 1 1 2 4 3 8 0 0 2 17 3 1 1 2 4 3 9 0 0 3 17 3 1 1 2 4 3 10 0 0 4 17 29 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 1 3 3 4 5 4 1 4 1 1 2 1 3 3 4 6 4 2 4 1 1 2 1 3 4 4 7 4 3 4 1 1 2 1 3 4 4 8 4 4 4 1 1 2 2 3 5 4 9 3 5 4 1 1 2 2 3 5 4 10 3 6 4 1 1 2 2 3 6 4 11 3 7 4 1 1 2 2 3 6 4 12 3 8 4 1 1 2 2 3 6 4 13 3 9 4 1 1 2 2 3 7 4 14 4 5 4 1 1 2 2 3 7 4 15 4 6 4 1 1 2 2 3 8 4 16 4 7 4 1 1 2 2 3 8 4 17 4 8 4 1 1 2 2 3 8 4 18 4 9 4 1 1 2 3 3 9 4 19 3 10 4 1 1 2 3 3 9 4 20 3 11 4 1 1 2 3 3 9 4 21 3 12 4 1 1 2 3 3 10 4 22 3 13 4 1 1 2 3 3 10 4 23 3 14 4 1 1 2 3 3 11 4 24 4 10 4 1 1 2 3 3 11 4 25 4 11 4 1 1 2 3 3 11 4 26 4 12 4 1 1 2 3 3 12 4 27 4 13 4 1 1 2 3 3 12 4 28 4 14 4 1 1 2 3 3 12 4 29 3 15 *************************************************** * 10. BRAKES *************************************************** 288 15 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 3 4 7 6 8 4 1 1 2 2 3 4 4 8 6 9 4 1 1 2 2 3 4 4 9 6 10 4 1 1 2 2 3 4 4 10 6 11 3 1 1 2 3 3 5 0 0 6 12 3 1 1 2 3 3 6 0 0 6 13 3 1 1 2 3 3 7 0 0 6 14 3 1 1 2 3 3 8 0 0 6 15 3 1 1 2 3 3 9 0 0 6 16 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 150 4 290 100 3 100 4 160 80 *************************************************** * 12. H V and VH ribs *************************************************** 3 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 9 1 10 1 2.5 0 0 0 ***************************************************** * 15. Extrados colors ***************************************************** 0 ***************************************************** * 16. Intrados colors ***************************************************** 0 ***************************************************** * 17. Aditional rib points ***************************************************** 0 ***************************************************** * 18. Elastic lines corrections ***************************************************** 100 70 30 40 40 20 32 32 22 14 30 30 20 12 8 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 DEFINITIONS (NYLON RODS) ******************************************************* 2 2 1 1 1 1 1 16 5.5 10. 1.5 2.0 5. 10. 2.2 2.0 0.0 9.35 6.3 9.35 2 2 1 1 1 12 61.37 6.61 81.34 3.03 0.6 0.0 9.35 6.3 9.35 ******************************************************* * 22. NOSE MYLARS DEFINITIONS ******************************************************* 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 30 orange C_lines_color 3 green D_lines_color 4 cyan E_lines_color 8 grey F_lines_color 5 blue Extrados 1 7 white 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 6 80 80 17 1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 3 10. 30.35 60 0 0 0 -4 9 4 9 ******************************************************* * 29. 3D SHAPING ******************************************************* 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 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 PART SEPARATION ******************************************************* 1 panel_x 1.0 panel_x_min 1.0 panel_y 0.4 rib_x 0.9 rib_y 0.5 parameter6 1.0 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0 1 panel_x 2.0 panel_x_min 3.0 panel_y 0.4 rib_x 1.2 rib_y 1.2 parameter6 1.0 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0