************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file version 3.15 * ************************************************************** * gnuA2-25 m2 Update 2021-07-24 ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "LABORATORI D'ENVOL" * Wing name "gnuA2" * Drawing scale 1. * Wing scale 0.9618 * Number of cells 28 * Number of ribs 30 * Alpha max and parameter 4.0 2 0 * Paraglider type and parameter "ds" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 .00 .00 309.33 .00 .00 .00 33.33 .00 2 46.87 .66 308.98 46.83 1.69 4.21 33.33 .00 3 93.42 2.64 307.94 93.10 6.69 8.12 33.33 .00 4 139.44 5.93 306.23 138.37 14.88 12.23 33.33 .00 5 184.71 10.51 303.83 182.25 26.03 16.34 33.33 .00 6 229.04 16.38 300.77 224.35 39.88 20.25 33.33 .00 7 272.21 23.53 297.05 264.18 56.48 25.21 33.33 .00 8 313.99 32.26 292.70 301.19 75.84 29.95 33.33 .00 9 353.99 44.10 287.74 334.95 97.27 34.70 33.33 .00 10 391.81 58.86 282.08 365.16 120.01 39.23 33.33 .00 11 427.13 76.06 275.68 391.55 143.45 45.06 33.33 .00 12 459.67 95.18 268.68 412.84 168.03 53.09 33.33 .00 13 489.23 115.70 261.24 429.04 192.73 60.45 33.33 .00 14 515.70 137.14 253.53 439.14 217.12 75.10 33.33 .00 15 539.00 159.09 245.71 442.53 240.90 88.27 33.33 .00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open , disp. rrw 1 gnua.txt 1.6 6.3 1 0 1 1 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 1 0 1 15 14 gnua.txt 1.6 6.3 0 0 1 15 15 gnuat.txt 0.0 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 3 9.0 35.0 60 0 0 100 13 3 9.9 38.0 65 0 0 100 14 3 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 16 0.01 ************************************************************* * 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 7.5 * Center of pressure % of chord 43 * Calage % 25 * Risers lenght cm 47 * Line lenght cm 680 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 4 6 3 1 1 2 1 3 1 0 0 1 2 3 1 1 2 1 3 2 0 0 1 4 3 1 1 2 2 3 3 0 0 1 6 3 1 1 2 2 3 4 0 0 1 8 3 1 1 2 3 3 5 0 0 1 10 3 1 1 2 3 3 6 0 0 1 12 12 3 1 1 2 1 3 1 0 0 2 2 3 1 1 2 1 3 2 0 0 2 4 3 1 1 2 2 3 3 0 0 2 6 3 1 1 2 2 3 4 0 0 2 8 3 1 1 2 3 3 5 0 0 2 10 3 1 1 2 3 3 6 0 0 2 12 3 1 1 2 4 3 7 0 0 1 14 3 1 1 2 4 3 8 0 0 2 14 3 1 1 2 4 3 9 0 0 1 15 3 1 1 2 4 3 10 0 0 2 15 3 1 1 2 4 3 11 0 0 3 15 3 1 1 2 4 3 12 0 0 4 15 6 3 1 1 2 1 3 1 0 0 3 2 3 1 1 2 1 3 2 0 0 3 4 3 1 1 2 2 3 3 0 0 3 6 3 1 1 2 2 3 4 0 0 3 8 3 1 1 2 3 3 5 0 0 3 10 3 1 1 2 3 3 6 0 0 3 12 5 3 1 1 2 1 3 1 0 0 4 2 3 1 1 2 1 3 2 0 0 4 4 3 1 1 2 2 3 3 0 0 4 6 3 1 1 2 2 3 4 0 0 4 8 3 1 1 2 2 3 5 0 0 4 10 *************************************************** * 10. BRAKES *************************************************** 270 9 3 1 1 2 1 3 1 0 0 6 3 3 1 1 2 1 3 2 0 0 6 4.5 3 1 1 2 1 3 3 0 0 6 6 3 1 1 2 2 3 4 0 0 6 7 3 1 1 2 2 3 5 0 0 6 8.5 3 1 1 2 2 3 6 0 0 6 10 3 1 1 2 3 3 7 0 0 6 11 3 1 1 2 3 3 8 0 0 6 12.5 3 1 1 2 3 3 9 0 0 6 14 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 160 4 300 150 3 135 4 200 80 *************************************************** * 12. H V and VH ribs *************************************************** 49 80 150 1 3 2 1 1 0 4.0 10 1 0 2 3 2 2 1 0 4.0 10 1 0 3 3 2 3 1 0 4.0 10 1 0 4 3 2 4 1 0 4.0 10 1 0 5 3 2 1 0 1 4.0 10 1 0 6 3 2 2 0 1 4.0 10 1 0 7 3 2 3 0 1 4.0 10 1 0 8 3 2 4 0 1 4.0 10 1 0 9 3 4 1 1 0 4.0 10 1 0 10 3 4 2 1 0 4.0 10 1 0 11 3 4 3 1 0 4.0 10 1 0 12 3 4 4 1 0 4.0 10 1 0 13 3 4 1 0 1 4.0 10 1 0 14 3 4 2 0 1 4.0 10 1 0 15 3 4 3 0 1 4.0 10 1 0 16 3 4 4 0 1 4.0 10 1 0 17 3 6 1 1 0 4.0 10 1 0 18 3 6 2 1 0 4.0 10 1 0 19 3 6 3 1 0 4.0 10 1 0 20 3 6 4 1 0 4.0 10 1 0 21 3 6 1 0 1 4.0 10 1 0 22 3 6 2 0 1 4.0 10 1 0 23 3 6 3 0 1 4.0 10 1 0 24 3 6 4 0 1 4.0 10 1 0 25 3 8 1 1 0 4.0 10 1 0 26 3 8 2 1 0 4.0 10 1 0 27 3 8 3 1 0 4.0 10 1 0 28 3 8 4 1 0 4.0 10 1 0 29 3 8 1 0 1 4.0 10 1 0 20 3 8 2 0 1 4.0 10 1 0 31 3 8 3 0 1 4.0 10 1 0 32 3 8 4 0 1 4.0 10 1 0 33 3 10 1 1 0 4.0 10 1 0 34 3 10 2 1 0 4.0 10 1 0 35 3 10 3 1 0 4.0 10 1 0 36 3 10 4 1 0 4.0 10 1 0 37 3 10 1 0 1 4.0 10 1 0 38 3 10 2 0 1 4.0 10 1 0 39 3 10 3 0 1 4.0 10 1 0 40 3 10 4 0 1 4.0 10 1 0 41 3 12 1 1 0 4.0 10 1 0 42 3 12 2 1 0 4.0 10 1 0 43 3 12 3 1 0 4.0 10 1 0 44 3 12 1 0 1 4.0 10 1 0 45 3 12 2 0 1 4.0 10 1 0 46 3 12 3 0 1 4.0 10 1 0 47 3 14 1 1 0 4.0 10 1 0 48 3 14 2 1 0 4.0 10 1 0 49 3 14 3 1 0 4.0 10 1 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 ***************************************************** 2 10.8 10.62 10.8 -4.76 ***************************************************** * 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 11 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 12 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 1 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0 9 0 10 0 11 0 12 0 13 0 14 -1 15 -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 14 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 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 0