************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file version 3.25 * ************************************************************** * Version update 20250107 * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "CRAZY BIRD" * Wing name "TULUAQ_19" * Drawing scale 1. * Wing scale 0.838404842 * Number of cells 34 * Number of ribs 35 * 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 0.00 -0.00 309.33 0.00 0.00 0.00 33.33 0.00 2 38.45 0.45 309.10 38.43 1.14 3.39 33.33 0.00 3 76.72 1.78 308.40 76.54 4.53 6.68 33.33 0.00 4 114.70 3.99 307.24 114.10 10.10 10.17 33.33 0.00 5 152.26 7.09 305.62 150.87 17.77 13.46 33.33 0.00 6 189.30 11.05 303.55 186.63 27.39 16.75 33.33 0.00 7 225.70 15.89 301.02 221.19 38.83 19.84 33.33 0.00 8 261.35 21.59 298.06 254.26 52.10 23.91 33.33 0.00 9 296.12 28.16 294.66 285.51 67.34 28.01 33.33 0.00 10 329.83 36.51 290.83 314.69 84.21 32.11 33.33 0.00 11 362.26 47.03 286.60 341.59 102.30 35.78 33.33 0.00 12 393.19 59.46 281.85 366.08 121.19 39.45 33.33 0.00 13 422.44 73.57 276.59 388.01 140.53 44.30 33.33 0.00 14 449.84 89.04 270.91 406.48 160.75 50.99 33.33 0.00 15 475.27 105.60 264.89 421.40 181.33 57.30 33.33 0.00 16 498.65 122.96 258.62 432.82 201.70 65.94 33.33 0.00 17 519.90 140.86 252.19 439.35 221.88 78.25 33.33 0.00 18 539.00 159.09 245.71 441.49 240.83 88.85 33.33 0.00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open , disp. rrw 1 gnua.txt 1.6 6.3 1 1.14 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 1.07 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 1.18 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 0.99 1 15 13 gnua.txt 1.6 6.3 1 0 1 15 14 gnua.txt 1.6 6.3 1 0 1 15 15 gnua.txt 1.6 6.3 1 1.40 1 15 16 gnua.txt 1.6 6.3 0 0 1 15 17 gnua.txt 1.6 6.3 0 2.01 1 15 18 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 4 8.6 27.5 53 77 0 100 14 4 8.6 27.5 53 77 0 100 15 4 8.6 27.5 53 77 0 100 16 4 8.6 27.5 53 77 0 100 17 4 8.6 27.5 53 77 0 100 18 4 0.0 30 60 90 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 1 17 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 10 upper panels (mm) 15 25 10 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 39 * Calage % 36 * Risers lenght cm 47 * Line lenght cm 680 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 3 10 4 1 1 2 1 3 1 4 1 1 2 4 1 1 2 1 3 1 4 2 1 3 4 1 1 2 1 3 1 4 3 1 4 4 1 1 2 1 3 2 4 4 1 6 4 1 1 2 1 3 2 4 5 1 7 4 1 1 2 1 3 2 4 6 1 8 4 1 1 2 2 3 3 4 7 1 10 4 1 1 2 2 3 3 4 8 1 11 4 1 1 2 2 3 4 4 9 1 13 4 1 1 2 2 3 4 4 10 1 14 18 4 1 1 2 1 3 1 4 1 2 2 4 1 1 2 1 3 1 4 2 2 3 4 1 1 2 1 3 1 4 3 2 4 4 1 1 2 1 3 2 4 4 2 6 4 1 1 2 1 3 2 4 5 2 7 4 1 1 2 1 3 2 4 6 2 8 4 1 1 2 2 3 3 4 7 2 10 4 1 1 2 2 3 3 4 8 2 11 4 1 1 2 2 3 4 4 9 2 13 4 1 1 2 2 3 4 4 10 2 14 3 1 1 2 3 3 5 0 0 1 16 3 1 1 2 3 3 6 0 0 1 18 3 1 1 2 3 3 7 0 0 2 16 3 1 1 2 3 3 8 0 0 2 18 3 1 1 2 3 3 9 0 0 3 16 3 1 1 2 3 3 10 0 0 3 18 3 1 1 2 3 3 11 0 0 4 16 3 1 1 2 3 3 12 0 0 4 18 20 4 1 1 2 1 3 1 4 1 3 2 4 1 1 2 1 3 1 4 2 3 3 4 1 1 2 1 3 1 4 3 3 4 4 1 1 2 1 3 2 4 4 4 2 4 1 1 2 1 3 2 4 5 4 3 4 1 1 2 1 3 2 4 6 4 4 4 1 1 2 1 3 3 4 7 3 6 4 1 1 2 1 3 3 4 8 3 7 4 1 1 2 1 3 3 4 9 3 8 4 1 1 2 1 3 4 4 10 4 6 4 1 1 2 1 3 4 4 11 4 7 4 1 1 2 1 3 4 4 12 4 8 4 1 1 2 2 3 5 4 13 3 10 4 1 1 2 2 3 5 4 14 3 11 4 1 1 2 2 3 6 4 15 4 10 4 1 1 2 2 3 6 4 16 4 11 4 1 1 2 2 3 7 4 17 3 13 4 1 1 2 2 3 7 4 18 3 14 4 1 1 2 2 3 8 4 19 4 13 4 1 1 2 2 3 8 4 20 4 14 *************************************************** * 10. BRAKES *************************************************** 270 8 4 1 1 2 1 3 1 4 1 6 3 4 1 1 2 1 3 1 4 2 6 5 4 1 1 2 1 3 2 4 3 6 7 4 1 1 2 1 3 2 4 4 6 9 4 1 1 2 2 3 3 4 5 6 11 4 1 1 2 2 3 3 4 6 6 13 4 1 1 2 2 3 4 4 7 6 15 4 1 1 2 2 3 4 4 8 6 17 * 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 *************************************************** 60 80 150 1 5 2 1 1 0 60.0 60.0 80. 7. 2 5 2 2 1 0 60.0 60.0 80. 7. 3 5 2 3 1 0 60.0 60.0 80. 7. 4 5 2 4 1 0 60.0 60.0 80. 7. 5 5 4 1 0 1 60.0 60.0 80. 7. 6 5 4 2 0 1 60.0 60.0 80. 7. 7 5 4 3 0 1 60.0 60.0 80. 7. 8 5 4 4 0 1 60.0 60.0 80. 7. 9 5 6 1 1 0 60.0 60.0 80. 7. 10 5 6 2 1 0 60.0 60.0 80. 7. 11 5 6 3 1 0 60.0 60.0 80. 7. 12 5 6 4 1 0 60.0 60.0 80. 7. 13 5 8 1 0 1 60.0 60.0 80. 7. 14 5 8 2 0 1 60.0 60.0 80. 7. 15 5 8 3 0 1 60.0 60.0 80. 7. 16 5 8 4 0 1 60.0 60.0 80. 7. 17 5 10 1 1 0 60.0 60.0 80. 7. 18 5 10 2 1 0 60.0 60.0 80. 7. 19 5 10 3 1 0 60.0 60.0 80. 7. 20 5 10 4 1 0 60.0 60.0 80. 7. 21 5 11 1 0 1 60.0 60.0 80. 7. 22 5 11 2 0 1 60.0 60.0 80. 7. 23 5 11 3 0 1 60.0 60.0 80. 7. 24 5 11 4 0 1 60.0 60.0 80. 7. 25 5 13 1 1 0 60.0 60.0 80. 7. 26 5 13 2 1 0 60.0 60.0 80. 7. 27 5 13 3 1 0 60.0 60.0 80. 7. 28 5 13 4 1 0 60.0 60.0 80. 7. 29 5 14 1 0 1 60.0 60.0 80. 7. 30 5 14 2 0 1 60.0 60.0 80. 7. 31 5 14 3 0 1 60.0 60.0 80. 7. 32 5 14 4 0 1 60.0 60.0 80. 7. 33 5 16 1 1 1 60.0 60.0 80. 7. 34 5 16 2 1 1 60.0 60.0 80. 7. 35 5 16 3 1 1 60.0 60.0 80. 7. 36 5 16 4 1 1 60.0 60.0 80. 7. 37 1 2 1 3 1 5.0 0. 0. 0. 38 1 3 1 4 1 5.0 0. 0. 0. 39 1 6 1 7 1 5.0 0. 0. 0. 40 1 7 1 8 1 5.0 0. 0. 0. 41 1 10 1 11 1 5.0 0. 0. 0. 42 1 13 1 14 1 5.0 0. 0. 0. 43 1 2 2 3 2 5.0 0. 0. 0. 44 1 3 2 4 2 5.0 0. 0. 0. 45 1 6 2 7 2 5.0 0. 0. 0. 46 1 7 2 8 2 5.0 0. 0. 0. 47 1 10 2 11 2 5.0 0. 0. 0. 48 1 13 2 14 2 5.0 0. 0. 0. 49 1 2 3 3 3 5.0 0. 0. 0. 50 1 3 3 4 3 5.0 0. 0. 0. 51 1 6 3 7 3 5.0 0. 0. 0. 52 1 7 3 8 3 5.0 0. 0. 0. 53 1 10 3 11 3 5.0 0. 0. 0. 54 1 13 3 14 3 5.0 0. 0. 0. 55 1 2 4 3 4 5.0 0. 0. 0. 56 1 3 4 4 4 5.0 0. 0. 0. 57 1 6 4 7 4 5.0 0. 0. 0. 58 1 7 4 8 4 5.0 0. 0. 0. 59 1 10 4 11 4 5.0 0. 0. 0. 60 1 13 4 14 4 5.0 0. 0. 0. ***************************************************** * 15. Extrados colors ***************************************************** 1 1 1 1 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 5 blue C_lines_color 30 orange D_lines_color 3 green E_lines_color 3 green F_lines_color 2 yellow ******************************************************* * 25. GENERAL 3D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 5 blue C_lines_color 30 orange D_lines_color 3 green E_lines_color 3 green F_lines_color 2 yellow Extrados 0 8 dark grey Vents 0 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 1 1 4 50 50 2 4 50 50 3 4 50 100 4 -4 0 100 5 4 0 100 6 0 7 0 8 -4 0 100 9 4 0 100 10 0 11 0 12 -4 0 100 13 4 0 100 14 0 15 0 16 -4 0 100 17 -1 18 -1 ******************************************************* * 27. SPECIAL WING TIP ******************************************************* 0 ******************************************************* * 28. PARAMETERS FOR CALAGE VARIATION ******************************************************* 1 3 8.5 27.5 53 77 0 0 -4 4 4 4 ******************************************************* * 29. 3D SHAPING ******************************************************* 1 1 groups 1 group 1 1 15 upper 0 1 lower 0 1 * Print parameters Inter3D 0 1 17 1 Ovali3D 0 1 17 0 tesse3D 1 1 18 1 exteDXF 1 1 18 1 exteSTL 1 1 18 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 9 0.9 10 0.9 11 0.9 12 0.9 13 0.9 14 0.9 15 0.9 16 0.9 17 0.8 18 0.1 (0.0 modified for XFLR5 convergence!!!) ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 18, 11 points, type "1" 1 1 18 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 ******************************************************* 0 ******************************************************* * 33. DETAILED RISERS ******************************************************* 1 1 A 47.0 cm B 47.0 cm C 47.0 cm ******************************************************* * 34. LINES CHARACTERISTICS TABLE ******************************************************* 1 6 1 r 12. 2.5 Riser 1000 daN aramid 15.0 g s 12. cm 7 2 c 1.80 TSL280 280 daN s_technora 2.26 g s 12. cm 1 3 c 1.15 PPSL120 120 daN s_dyneem 1.00 g s 10. cm 30 4 c 0.9 PPSL65 65 daN s_dyneem 0.7 g s 10. cm 5 5 c 0.80 DSL70 70 daN u_dyneem 0.43 g p 8. cm 7 6 c 2.00 DSL350 350 daN s_dynemm 3.10 g s 12. cm 6 ******************************************************* * 35. SOLVE EQUILIBRIUM EQUATIONS ******************************************************* 0 ******************************************************* * 36. CREATE FILES FOR XFLR5 ANALYSIS ******************************************************* 1 * Panel parameters 80 chord nr 2 per cell 1 cosine distribution along chord 0 uniform along span * Include billowed airfoils (more accuracy) 0 ******************************************************* * 37. SOME SPECIAL PARAMETERS ******************************************************* 1 1 10291 10 nsegments in transverse direction (stl surfaces)