AGDISP Input Data Summary Title: APVMA AGDISP - Aircraft - Fixed-Wing - 19Sept2015 Notes: Calculations Done: Yes Run ID: AGDISP APVMA AGDISP - Aircraft - Fixed-Wing - 19Sept2015.ag 8.28 09-19-2015 13:12:52 --APPLICATION METHOD-- ---------------------------- Method Aerial --Aircraft-- ---------------------------- Name Air Tractor AT-502B Type Library Wing Type Fixed-Wing Semispan (m) 7.92 Weight (kg) 3173.88 Typical Speed (m/s) 60.35 Propeller RPM 2000 Propeller Radius (m) 1.34 Biplane Separation (m) 0 Planform Area (m²) 28.99 Engines 1 Engine Vert Distance (m) 0 Engine Fwd Distance (m) 4.19 Engine Horiz Distance 1 (m) 0 Engine Horiz Distance 2 (m) 0 Wing Vertical Distance (m) 0.4694 Boom Vertical Distance (m) -0.2012 Boom Forward Distance (m) -0.1524 --Spray Lines-- ---------------------------- Release Height (m) 3 Spray Lines 25 Optimize Spray Reps No Spray Line Reps # Reps 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 1 14 1 15 1 16 1 17 1 18 1 19 1 20 1 21 1 22 1 23 1 24 1 25 1 --APPLICATION TECHNIQUE-- ---------------------------- Application Technique Liquid --Nozzles-- ---------------------------- Boom Length (%) 70 Nozzle Locations # Hor(m) Ver(m) Fwd(m) 1 -5.54 0 0 2 -5.29 0 0 3 -5.03 0 0 4 -4.77 0 0 5 -4.51 0 0 6 -4.25 0 0 7 -4 0 0 8 -3.74 0 0 9 -3.48 0 0 10 -3.22 0 0 11 -2.97 0 0 12 -2.71 0 0 13 -2.45 0 0 14 -2.19 0 0 15 -1.93 0 0 16 -1.68 0 0 17 -1.42 0 0 18 -1.16 0 0 19 -0.9025 0 0 20 -0.6447 0 0 21 -0.3868 0 0 22 -0.1289 0 0 23 0.1289 0 0 24 0.3868 0 0 25 0.6447 0 0 26 0.9025 0 0 27 1.16 0 0 28 1.42 0 0 29 1.68 0 0 30 1.93 0 0 31 2.19 0 0 32 2.45 0 0 33 2.71 0 0 34 2.97 0 0 35 3.22 0 0 36 3.48 0 0 37 3.74 0 0 38 4 0 0 39 4.25 0 0 40 4.51 0 0 41 4.77 0 0 42 5.03 0 0 43 5.29 0 0 44 5.54 0 0 --Drop Size Distribution-- ---------------------------- Name APVMA F-M Type User-defined Drop Categories # Diam (um) Frac 1 4.00 0.0001 2 4.40 0.0000 3 4.80 0.0000 4 5.20 0.0000 5 5.70 0.0000 6 6.20 0.0000 7 6.70 0.0000 8 7.30 0.0000 9 8.00 0.0001 10 8.70 0.0001 11 9.50 0.0001 12 10.40 0.0001 13 11.30 0.0001 14 12.30 0.0001 15 13.50 0.0002 16 14.70 0.0002 17 16.00 0.0002 18 17.40 0.0003 19 19.00 0.0003 20 20.70 0.0004 21 22.60 0.0005 22 24.70 0.0006 23 26.90 0.0007 24 29.30 0.0009 25 32.00 0.0011 26 34.90 0.0013 27 38.10 0.0016 28 41.50 0.0018 29 45.30 0.0023 30 49.40 0.0027 31 53.80 0.0032 32 58.70 0.0039 33 64.00 0.0046 34 69.80 0.0056 35 76.10 0.0067 36 83.00 0.0080 37 90.50 0.0096 38 98.70 0.0114 39 108.00 0.0142 40 117.00 0.0149 41 128.00 0.0197 42 140.00 0.0233 43 152.00 0.0250 44 166.00 0.0311 45 181.00 0.0354 46 197.00 0.0397 47 215.00 0.0465 48 235.00 0.0532 49 256.00 0.0567 50 279.00 0.0618 51 304.00 0.0654 52 332.00 0.0695 53 362.00 0.0685 54 395.00 0.0667 55 431.00 0.0615 56 470.00 0.0533 57 512.00 0.0430 58 558.00 0.0327 59 609.00 0.0228 60 664.00 0.0138 61 724.00 0.0074 62 790.00 0.0033 63 861.00 0.0012 64 939.00 0.0004 65 1024.00 0.0001 66 1117.00 0.0000 67 1218.00 0.0000 68 1328.00 0.0000 69 1448.00 0.0000 70 1579.00 0.0000 71 1722.00 0.0000 72 1878.00 0.0000 73 2048.00 0.0000 74 2233.00 0.0000 75 2435.00 0.0000 76 2656.00 0.0000 77 2896.00 0.0000 78 3158.00 0.0000 79 3444.00 0.0000 --SWATH-- ---------------------------- Swath Width 20 m Swath Displacement 0 m --METEOROLOGY-- ---------------------------- Wind Speed (m/s) 5.56 Wind Direction (deg) -90 Temperature (deg C) 25 Relative Humidity (%) 30 --SPRAY MATERIAL-- ---------------------------- Name Water Spray Material Evaporates Yes Spray Volume Rate (L/ha) 20 Active Fraction 0.05 Nonvolatile Fraction 0.05 Active Fraction of Tank Mix 0.05 Fraction of Active Solution that is Nonvolatile 1 Additive Fraction of Tank Mix 0 Fraction of Additive Solution that is Nonvolatile 1 --ATMOSPHERIC STABILITY-- ---------------------------- Atmospheric Stability Overcast --SURFACE-- ---------------------------- Upslope Angle (deg) 0 Sideslope Angle (deg) 0 --Canopy-- ---------------------------- Type None Surface Roughness (m) 0.0075 --TRANSPORT-- ---------------------------- Flux Plane Distance (m) 0 --ADVANCED SETTINGS-- ---------------------------- Wind Speed Height (m) 2 Max Compute Time (sec) 600 Max Downwind Dist (m) 802 Vortex Decay Rate (OGE) (m/s) 0.15 Vortex Decay Rate (IGE) (m/s) 0.56 Aircraft Drag Coeff 0.1 Propeller Efficiency 0.8 Ambient Pressure (mb) 1013 Ground Reference (m) 0 Save Trajectory Files No Half Boom No Default Swath Offset 1/2 Swath Specific Gravity (Carrier) 1 Specific Gravity (Active/Additive) 1 Evaporation Rate (µm²/deg C/sec) 40