************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file * ************************************************************** * Version 20180902 (uses especial version LEP-2.77) ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "GNU19-v3-2018" * Drawing scale 1.0 * Wing scale 1.0 * Number of cells 23 * Number of ribs 24 * Alpha wingtip, parameter, (alpha center) 8.0 0 0.0 * Paraglider type and parameter "ss" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 19.74 .00 250.00 19.73 .25 1.48 33.33 .00 2 59.21 .02 249.98 59.15 2.27 4.45 33.33 .00 3 98.68 .07 249.93 98.41 6.31 7.32 33.33 .00 4 138.16 .13 249.87 137.42 12.35 10.45 33.33 .00 5 177.63 .22 249.78 175.81 21.46 16.23 33.33 .10 6 217.11 3.43 249.54 213.08 34.42 22.14 33.33 .20 7 255.58 11.78 248.56 247.75 51.03 29.22 33.33 1.50 8 294.05 25.21 246.74 280.02 71.93 36.72 33.33 3.00 9 331.53 43.45 244.09 308.63 96.09 43.72 33.33 4.00 10 367.00 65.71 240.75 332.26 122.48 55.34 33.33 5.00 11 399.00 89.56 237.10 346.72 150.91 70.83 33.33 6.00 12 425.00 122.74 233.74 352.69 178.89 83.68 33.33 8.00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name. intake in. intake out. open. disp rweight 1 gnuPSF.txt 2.244 10.0 1 0 1 1 2 gnuPSF.txt 2.244 10.0 1 0 1 1 3 gnuPSF.txt 2.244 10.0 1 0 1 1 4 gnuPSF.txt 2.244 10.0 1 0 1 1 5 gnuPSF.txt 2.244 10.0 1 0 1 1 6 gnuPSF.txt 2.244 10.0 1 0 1 1 7 gnuPSF.txt 2.244 10.0 1 0 1 1 8 gnuPSF.txt 2.244 10.0 1 0 1 1 9 gnuPSF.txt 2.244 10.0 1 0 1 1 10 gnuPSFtube.txt 2.244 10.0 1 0 1 0 11 gnuPSFtube.txt 2.244 10.0 1 0 1 0 12 gnuPSFtube.txt 2.244 10.0 1 0 1 0 ************************************************************* * 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 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 11 11 5 1 16.68 3.5 5.28 5.28 0. 0. 0. 1 32.26 3.5 4.71 4.71 0. 0. 0. 1 46.91 3.14 4.17 4.17 0. 0. 0. 1 60.06 2.96 2.85 2.85 0. 0. 0. 1 70.30 2.31 2.06 2.06 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. 0.0001 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 4.4 * Center of pressure % of chord 35 * Calage % 25 * Risers lenght cm 47 * Line lenght cm 500 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 3 10 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 3 3 10 0 0 1 10 14 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 3 3 10 0 0 2 10 3 1 1 2 4 3 11 0 0 1 12 3 1 1 2 4 3 12 0 0 2 12 3 1 1 2 4 3 13 0 0 3 12 3 1 1 2 4 3 14 0 0 4 12 20 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 3 10 3 1 1 2 3 3 17 0 0 4 7 3 1 1 2 3 3 18 0 0 4 8 3 1 1 2 3 3 19 0 0 4 9 3 1 1 2 3 3 20 0 0 4 10 *************************************************** * 10. BRAKES *************************************************** 200 6 3 1 1 2 1 3 1 0 0 6 1 3 1 1 2 1 3 2 0 0 6 3 3 1 1 2 1 3 3 0 0 6 5 3 1 1 2 2 3 4 0 0 6 7 3 1 1 2 2 3 5 0 0 6 9 3 1 1 2 2 3 6 0 0 6 11 * Brake distribution 0 25 50 80 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 275 100 3 135 4 200 80 *************************************************** * 12. H V and VH ribs *************************************************** 1 80 150 1 5 2 1 1 1 50. 35. 85. 4.5 ***************************************************** * 15. Extrados colors ***************************************************** 3 1 1 1 40 0. 2 1 1 20 0. 3 1 1 0.0 0. ***************************************************** * 16. Intrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 17. Aditional rib points ***************************************************** 2 8.288 7.27 11.21 -2.113 ***************************************************** * 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 2.5 1.2 2 0.2 1.2 typepoint2 1 2.5 1.2 2 0.2 1.2 typepoint3 1 2.5 1.2 2 0.2 1.2 typevent 1 0. 0.0 1 10. 2.0 typetab 1 0. 0.0 3 2.0 1.0 typejonc 1 0. 0.0 2 2.0 0.0 typeref 1 5. 1. 1 2.0 0.0 type8 1 0.25 1.2 2 0.2 1.2 type9 1 0.25 1.2 2 0.2 1.2 type10 1 0.25 1.2 2 0.2 1.2 ******************************************************* * 21. JONCS DEFINITION (NYLON RODS) ******************************************************* 0 ******************************************************* * 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 1 1 red Intrados 0 3 green ******************************************************* * 26. GLUE VENTS ******************************************************* 0 ******************************************************* * 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 ******************************************************* 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 0.0 ******************************************************* * 31. NEW SKIN TENSION MODULE (not implemented in 2.75) ******************************************************* 1 3 * Skin tension group number "1" from rib 1 to 4, 6 points, type "1" 1 1 4 6 1 1 0. 0.0 0. 0. 2 7.5 1.3 10. 1.33 3 15. 2.5 20. 2.5 4 80. 2.5 80. 2.5 5 90. 1.33 90. 1.33 6 100. 0.0 100. 0. * Skin tension group number "2" from rib 5 to 22, 6 points, type "1" 2 5 22 6 1 1 0. 0.0 0. 0. 2 7.5 1.3 10. 1.33 3 15. 2.5 20. 2.5 4 80. 2.5 80. 2.5 5 90. 1.33 90. 1.33 6 100. 0.0 100. 0. * Skin tension group number "3" from rib 22 to 23, 8 points, type "1" 3 22 23 8 1 1 0. 0.0 0. 0. 2 7.5 1.3 10. 1.33 3 15. 2.5 20. 2.5 4 50. 2.5 60. 2.5 5 65. 2.5 70. 2.5 6 75. 2.0 80. 1.9 7 90 1.0 90 1.0 8 100. -1.0 100. -1.0 ********************************************************