* Brand name "Pyren-Wings" * Wing name "Chooca-15" * Drawing scale 1. * Wing scale 0.80970 * Number of cells 25 * Number of ribs 26 * Alpha max and parameter 6.5 0 * Paraglider type and parameter "ss" 1 * Rib geometric parameters Rib x-rib y-LE y-TE xp z beta RP Washin rot-z % 1 26.13 0.19 267.99 26.13 0.47 2.05 33.33 0.01 0.25 50.00 2 78.10 1.66 267.17 77.95 4.21 6.17 33.33 0.04 0.75 50.00 3 129.48 4.59 265.54 128.79 11.54 10.28 33.33 0.11 1.24 50.00 4 179.96 8.98 263.11 178.10 22.29 14.80 33.33 0.23 1.78 50.00 5 229.25 14.83 259.90 225.08 37.15 20.44 33.33 0.44 2.43 50.00 6 277.07 22.14 255.91 269.04 55.91 25.82 33.33 0.7 3.03 50.00 7 323.06 31.42 251.19 309.45 77.84 31.20 33.33 1.01 3.60 50.00 8 366.65 44.39 245.79 345.73 101.98 36.07 33.33 1.33 4.09 50.00 9 407.30 60.72 239.63 377.35 127.49 42.58 33.33 1.83 4.70 50.00 10 444.54 79.78 232.59 403.02 154.43 50.13 33.33 2.49 5.33 50.00 11 478.01 100.96 224.94 422.85 181.36 57.08 33.33 3.17 5.82 50.00 12 507.45 123.75 216.95 435.58 207.78 73.51 33.33 4.97 6.65 50.00 13 532.69 150.00 212.00 439.34 234.90 89.35 33.33 6.85 6.93 50.00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open, disp, rrw 1 choocairfoil4p.txt 2.244 10.0 1 0 1 1 2 choocairfoil4p.txt 2.244 10.0 1 0 1 1 3 choocairfoil4p.txt 2.244 10.0 1 0 1 1 4 choocairfoil4p.txt 2.244 10.0 1 0 1 1 5 choocairfoil4p.txt 2.244 10.0 1 0 1 1 6 choocairfoil4p.txt 2.244 10.0 1 0 1 1 7 choocairfoil4p.txt 2.244 10.0 1 0 1 1 8 choocairfoil4p.txt 2.244 10.0 1 0 1 1 9 choocairfoil4p.txt 2.244 10.0 1 0 1 1 10 choocairfoil4p.txt 2.244 10.0 1 0 1 1 11 choocairfoil4p.txt 2.244 10.0 1 0 1 1 12 chooca-inflate.txt 2.244 10.0 1 0 1 1 13 chooca-inflate.txt 0.000 0.00 1 0 1 1 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 4 10. 30.35 51.32 75.28 0 100 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 3 10. 45.00 85.00 0 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 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 40 * Calage % 34.85 * Risers lenght cm 47 * Line lenght cm 600 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 3 3 12 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 3 3 5 4 9 1 9 4 1 1 2 3 3 5 4 10 1 10 4 1 1 2 3 3 6 4 11 1 11 4 1 1 2 3 3 6 4 12 1 12 15 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 3 3 5 4 9 2 9 4 1 1 2 3 3 5 4 10 2 10 4 1 1 2 3 3 6 4 11 2 11 4 1 1 2 3 3 6 4 12 2 12 3 1 1 2 4 3 7 0 0 1 13 3 1 1 2 4 3 8 0 0 2 13 3 1 1 2 4 3 9 0 0 3 13 24 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 7 4 13 4 5 4 1 1 2 2 3 7 4 14 4 6 4 1 1 2 2 3 8 4 15 4 7 4 1 1 2 2 3 8 4 16 4 8 4 1 1 2 3 3 9 4 17 3 9 4 1 1 2 3 3 9 4 18 3 10 4 1 1 2 3 3 10 4 19 3 11 4 1 1 2 3 3 10 4 20 3 12 4 1 1 2 3 3 11 4 21 4 9 4 1 1 2 3 3 11 4 22 4 10 4 1 1 2 3 3 12 4 23 4 11 4 1 1 2 3 3 12 4 24 4 12 *************************************************** * 10. BRAKES *************************************************** 300 11 3 1 1 2 1 3 1 0 0 6 2 3 1 1 2 1 3 2 0 0 6 3 3 1 1 2 1 3 3 0 0 6 4 3 1 1 2 1 3 4 0 0 6 5 3 1 1 2 2 3 5 0 0 6 6 3 1 1 2 2 3 6 0 0 6 7 3 1 1 2 2 3 7 0 0 6 8 3 1 1 2 2 3 8 0 0 6 9 3 1 1 2 3 3 9 0 0 6 10 3 1 1 2 3 3 10 0 0 6 11 3 1 1 2 3 3 11 0 0 6 12 * Brake distribution 0 35 50 65 100 0 0 0 0 5 *************************************************** * 11. Ramification lengths *************************************************** 3 250 4 330 100 3 150 4 160 80 *************************************************** * 12. H V and VH ribs *************************************************** 1 80 150 1 1 0 1 1 1 2.5 0 0 0 ***************************************************** * 15. Extrados colors ***************************************************** 13 1 1 1 90 0 2 1 1 80 0 3 1 1 70 0 4 1 1 90 0 5 1 1 80 0 6 1 1 70 0 7 1 1 90 0 8 1 1 80 0 9 1 1 70 0 10 1 1 90 0 11 1 1 70 0 12 1 1 43 0 13 1 1 0.0 0 ***************************************************** * 16. Intrados colors ***************************************************** 0 ***************************************************** * 17. Aditional rib points ***************************************************** 0 ***************************************************** * 18. Elastic lines corrections ***************************************************** 80 70 30 58 28 14 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) ******************************************************* 1 1 1 1 12 5.5 10. 1.5 2.0 5. 10. 2.2 2.0 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 4 cyan C_lines_color 3 green D_lines_color 6 purple E_lines_color 5 blue F_lines_color 2 yellow ******************************************************* * 25. GENERAL 3D DXF OPTIONS ******************************************************* 1 A_lines_color 1 red B_lines_color 4 cyan C_lines_color 3 green D_lines_color 6 purple E_lines_color 5 blue F_lines_color 2 yellow 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 6 80 80 ******************************************************* * 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 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE ******************************************************* 1 1 * Skin tension group number "1" from rib 1 to 13, 14 points, type "1" 1 1 13 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 1.5 panel_x_min 2.0 panel_y 0.6 rib_x 1.1 rib_y 1.0 rib_1y 1.8 parameter7 1.0 parameter8 1.0 parameter9 1.0 parameter10 1.0 ******************************************************* * 33. DETAILED RISERS ******************************************************* 1 1 A 45.0 cm B 50.0 cm C 60.0 cm ******************************************************* * 34. LINES CHARACTERISTICS TABLE ******************************************************* 1 6 1 c 5.0 Riser 1000 daN dyneema 4.50 g p 14. cm 0 2 c 1.60 sus2 350 daN dyneema 1.68 g p 10. cm 0 3 c 1.30 sus3 250 daN dyneema 1.38 g p 10. cm 0 4 c 1.00 sus4 160 daN dyneema 0.76 g p 10. cm 0 5 c 0.80 sus5 100 daN dyneema 0.40 g p 10. cm 0 6 c 2.00 brake 440 daN dyneema 1.78 g p 10. cm 0 ******************************************************* * 35. SOLVE EQUILIBRIUM EQUATIONS ******************************************************* 0 ******************************************************* * 36. CREATE FILES FOR XFLR5 ANALYSIS ******************************************************* 0 ******************************************************* * 37. SOME SPECIAL PARAMETERS ******************************************************* 0