************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file version 3.19 * ************************************************************** * Version 2022-05-22 gnu-test-3.19 * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "LABORATORI D'ENVOL" * Wing name "gnu-test-3.19" * Drawing scale 1. * Wing scale 0.980762046 * Number of cells 29 * Number of ribs 30 * Alpha max and parameter 4.5 1 * Paraglider type and parameter "ds" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 22.65 0.16 309.25 22.64 0.40 1.95 33.33 0.00 0.0 50.0 2 67.75 1.39 308.60 67.62 3.53 6.06 33.33 0.00 0.0 50.0 3 112.46 3.84 307.32 111.90 9.71 9.97 33.33 0.00 0.0 50.0 4 156.60 7.50 305.40 155.09 18.79 13.87 33.33 0.00 0.0 50.0 5 199.98 12.37 302.86 196.84 30.55 17.57 33.33 0.00 0.0 50.0 6 242.42 18.43 299.70 236.81 44.75 21.75 33.33 0.00 0.0 50.0 7 283.72 25.69 295.93 274.49 61.65 26.50 33.33 0.00 0.0 50.0 8 323.64 34.78 291.58 309.41 80.96 31.25 33.33 0.00 0.0 50.0 9 361.82 46.86 286.67 341.23 102.04 35.78 33.33 0.00 0.0 50.0 10 397.91 61.58 281.06 369.71 124.21 40.10 33.33 0.00 0.0 50.0 11 431.64 78.51 274.77 394.47 147.07 46.40 33.33 0.00 0.0 50.0 12 462.75 97.17 267.95 414.34 170.99 54.04 33.33 0.00 0.0 50.0 13 491.09 117.10 260.74 429.49 194.91 61.64 33.33 0.00 0.0 50.0 14 516.52 137.86 253.27 438.60 218.59 76.24 33.33 0.00 0.0 50.0 15 539.00 159.09 245.71 441.49 240.83 88.85 33.33 0.00 0.0 50.0 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open , disp. rrw 1 gnua.txt 1.6 6.3 1 0 1 15 2 gnua.txt 1.6 6.3 1 0 1 15 3 gnua.txt 1.6 6.3 1 0 1 15 4 gnua.txt 1.6 6.3 1 0 1 15 5 gnua.txt 1.6 6.3 1 0 1 15 6 gnua.txt 1.6 6.3 1 0 1 15 7 gnua.txt 1.6 6.3 1 0 1 15 8 gnua.txt 1.6 6.3 1 0 1 15 9 gnua.txt 1.6 6.3 1 0 1 15 10 gnua.txt 1.6 6.3 1 0 1 15 11 gnua.txt 1.6 6.3 1 0 1 15 12 gnua.txt 1.6 6.3 1 0 1 15 13 gnua.txt 1.6 6.3 0 0 1 15 14 gnua.txt 1.6 6.3 0 0 1 15 15 gnua.txt 1.6 6.3 0 0 1 1 ************************************************************* * 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 8.6 27.5 53 77 0 100 12 4 8.6 27.5 53 77 0 100 13 3 9.9 40.0 75 0 0 100 14 0 9.9 40.0 75 0 0 100 15 4 0.0 30 60 90 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 2 1 12 9 1 14.59 2.79 2.735 6.72 0. 0. 0. 0. 1 22.18 2.61 2.375 6.72 0. 0. 0. 0. 1 33.36 1.64 2.5 5.9 0. 0. 0. 0. 1 40.32 1.46 2.4 5.8 0. 0. 0. 0. 1 47.41 1.34 2.23 5.7 0. 0. 0. 0. 1 59.17 1.27 1.84 3.4 0. 0. 0. 0. 1 65.23 1.33 1.7 3.2 0. 0. 0. 0. 1 71.21 1.18 1.6 3.0 0. 0. 0. 0. 1 81.87 0.89 1.6 1.6 0. 0. 0. 0. 13 14 3 1 23.5 2.5 6.5 6.5 0. 0. 0. 0. 1 55.0 1.92 4.3 4.3 0. 0. 0. 0. 1 81. 1.1 1.7 1.7 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 * ************************************************************* 15 25 25 upper panels (mm) 15 25 25 lower panels (mm) 15 ribs (mm) 15 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.5 0.15 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 7.0 * Center of pressure % of chord 35 * Calage % 25 * Risers lenght cm 47 * Line lenght cm 680 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 3 13 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 4 3 13 0 0 1 13 17 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 4 3 13 0 0 2 13 3 1 1 2 5 3 14 0 0 1 15 3 1 1 2 5 3 15 0 0 2 15 3 1 1 2 5 3 16 0 0 3 15 3 1 1 2 5 3 17 0 0 4 15 25 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 1 3 4 0 0 4 1 3 1 1 2 1 3 5 0 0 4 2 3 1 1 2 1 3 6 0 0 4 3 3 1 1 2 2 3 7 0 0 3 4 3 1 1 2 2 3 8 0 0 3 5 3 1 1 2 2 3 9 0 0 3 6 3 1 1 2 2 3 10 0 0 4 4 3 1 1 2 2 3 11 0 0 4 5 3 1 1 2 2 3 12 0 0 4 6 3 1 1 2 3 3 13 0 0 3 7 3 1 1 2 3 3 14 0 0 3 8 3 1 1 2 3 3 15 0 0 3 9 3 1 1 2 3 3 16 0 0 4 7 3 1 1 2 3 3 17 0 0 4 8 3 1 1 2 3 3 18 0 0 4 9 3 1 1 2 4 3 19 0 0 3 10 3 1 1 2 4 3 20 0 0 3 11 3 1 1 2 4 3 21 0 0 3 12 3 1 1 2 4 3 22 0 0 3 13 3 1 1 2 4 3 23 0 0 4 10 3 1 1 2 4 3 24 0 0 4 11 3 1 1 2 4 3 25 0 0 4 12 *************************************************** * 10. BRAKES *************************************************** 270 13 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 6 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 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 300 150 3 100 4 200 80 *************************************************** * 12. H V and VH ribs *************************************************** 16 80 150 1 1 0 1 1 1 6.0 0 0 0 2 1 0 2 1 2 6.0 0 0 0 3 1 0 3 1 3 6.0 0 0 0 4 1 0 4 1 4 6.0 0 0 0 5 1 3 1 4 1 6.0 0 0 0 6 1 3 2 4 2 6.0 0 0 0 7 1 3 3 4 3 6.0 0 0 0 8 1 3 4 4 4 6.0 0 0 0 9 1 6 1 7 1 6.0 0 0 0 10 1 6 2 7 2 6.0 0 0 0 11 1 6 3 7 3 6.0 0 0 0 12 1 6 4 7 4 6.0 0 0 0 13 1 9 1 10 1 6.0 0 0 0 14 1 9 2 10 2 6.0 0 0 0 15 1 9 3 10 3 6.0 0 0 0 16 1 9 4 10 4 6.0 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 ***************************************************** 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 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 10 4.2 10.8 1.36 2.0 3.67 10.8 0.79 2.0 0.0 9.35 6.3 9.35 2 11 14 4.2 10.8 1.36 2.0 3.67 10.8 0.79 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 0 5 blue Vents 0 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 -6 70 100 2 -4 0 80 3 -4 80 0 4 -4 0 80 5 -4 80 0 6 -4 0 100 7 -4 100 50 8 -4 50 0 9 4 100 0 10 5 0. 0. 80. 11 5 0. 0. 80. 12 -5 50. 50. 50. 13 -5 50. 100. 50. 14 -6 70. 70. 15 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 4 8.5 27.5 53 77 0 0 -4 4 4 4 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 2 group 1 1 10 upper 2 1 1 25 33 0.8 2 33 44 -0.3 lower 1 1 1 79 84 1.0 group 2 11 14 upper 2 1 1 25 33 0.9 2 33 44 0.9 lower 1 1 1 79 83 1.0 * Print parameters Inter3D 0 1 14 0 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 0.9 2 0.9 3 0.9 4 0.9 5 0.9 6 0.9 7 0.9 8 0.9 9 0.9 10 0.9 11 0.9 12 0.9 13 0.9 14 0.8 15 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 15, 11 points, type "1" 1 1 15 11 1 1 0. 0.05 0. 0. 2 3.5 0.1 10. 0.525 3 7.0 0.5 20. 1.25 4 14. 1.3 30. 1.875 5 19 2.38 35 2.1875 6 21.5 2.6 40. 2.5 7 65. 2.6 65. 2.5 8 72.5 2.4 70. 2.4 9 80. 2.0 75. 2.3 10 90. 0.8 87.5 1.15 11 100. 0.0 100. 0.1 ******************************************************* * 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