************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file version 3.16 * ************************************************************** * Version 2021-08-22 Rotations-Test * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "LABORATORI D'ENVOL" * Wing name "Rotations-Test" * Drawing scale 1.0 * Wing scale 1.0 * Number of cells 15 * Number of ribs 16 * Alpha max and parameter 0.0 0 * Paraglider type and parameter "ds" 1 * Rib geometric parameters. Extended data with two additional columns for "Z" versions (!) * Rib x-rib y-LE y-TE xp z beta RP Washin Rot_z Pos_z 1 41.72 0.42 270.76 41.69 1.16 0.00 33.33 0.00 0.00 50.0 2 124.64 3.78 268.69 124.07 10.33 10.00 33.33 3.00 1.95 50.0 3 206.57 10.51 264.57 203.97 28.27 15.00 33.33 6.00 2.91 50.0 4 286.98 20.74 258.41 279.31 56.16 25.00 33.33 10.00 4.75 50.0 5 365.35 34.64 250.23 347.87 93.98 30.00 33.33 15.00 5.63 50.0 6 440.64 57.63 239.83 407.14 140.22 45.00 33.33 20.00 7.97 50.0 7 511.15 96.61 227.18 453.42 193.28 50.00 33.33 25.00 8.64 50.0 8 575.50 148.95 212.80 473.45 254.62 90.00 33.33 30.00 11.31 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 ************************************************************* * 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 30 60 90 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 1 7 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. ************************************************************* * 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 5.0 * Center of pressure % of chord 32 * Calage % 22 * Risers lenght cm 47 * Line lenght cm 680 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 2 14 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 1 3 4 0 0 2 1 3 1 1 2 1 3 5 0 0 2 2 3 1 1 2 1 3 6 0 0 2 3 3 1 1 2 2 3 7 0 0 1 4 3 1 1 2 2 3 8 0 0 1 5 3 1 1 2 2 3 9 0 0 1 6 3 1 1 2 2 3 10 0 0 1 7 3 1 1 2 2 3 11 0 0 2 4 3 1 1 2 2 3 12 0 0 2 5 3 1 1 2 2 3 13 0 0 2 6 3 1 1 2 2 3 14 0 0 2 7 18 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 3 7 3 1 1 2 2 3 11 0 0 4 4 3 1 1 2 2 3 12 0 0 4 5 3 1 1 2 2 3 13 0 0 4 6 3 1 1 2 2 3 14 0 0 4 7 3 1 1 2 3 3 15 0 0 1 8 3 1 1 2 3 3 16 0 0 2 8 3 1 1 2 3 3 17 0 0 3 8 3 1 1 2 3 3 18 0 0 4 8 *************************************************** * 10. BRAKES *************************************************** 270 7 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 1 4 3 6 4 4 1 1 2 2 3 2 4 4 6 5 4 1 1 2 2 3 2 4 5 6 6 4 1 1 2 2 3 2 4 6 6 7 4 1 1 2 2 3 2 4 7 6 8 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 230 4 300 150 3 100 4 200 100 *************************************************** * 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 2 2 1 1 1 3.0 5.0 80. 90. 10 3 2 2 1 1 3.0 5.0 0. 0. 11 4 2 3 1 1 3.0 5.0 80. 90. 12 5 5 1 1 1 60. 40. 77. 4. 13 5 5 2 1 1 60. 40. 77. 4. 14 5 5 3 1 1 60. 40. 77. 4. 15 5 5 4 1 1 60. 40. 77. 4. 16 6 6 50. 0. 3. 3. 7 50. 100. 7. 7. ***************************************************** * 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 0.25 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 1 5 blue Vents 0 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 3 10. 30.35 60 0 0 0 -4 4 4 4 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 8 upper 0 1 lower 0 1 * Print parameters Inter3D 0 1 7 1 Ovali3D 0 1 7 0 tesse3D 0 1 7 0 exteDXF 0 1 7 0 exteSTL 0 1 7 0 ******************************************************* * 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 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 8, 11 points, type "1" 1 1 8 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