choisizingconcept_carpet_plot(1)

choisizingconcept_carpet_plot(1) - Fuselage Nose Length...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: Fuselage Nose Length y­location diameter Number of Passengers Number of Flight Crew Mcruise Center of Gravity x­location Neutral Point x­location Static Margin #NUM! Chord Empty Weight Total Weight Thrust To Weight Ratio Wing Loading 11 ­2 0 Fuselage Empannage End 27 0 7 13 0 7 9 2 0.800 #NUM! #NUM! #NUM! #NUM! #NUM! 0.3 70 ft ft #NUM! lb lb 0 2 0 Wing Area Leading Edge Angle Sweep Angle Taper Ratio Aspect Ratio x­Location y­Location Main Wing #NUM! 30 #NUM! 0.5 7.8 22 ­3 NACA Wing Canard 0 25 #DIV/0! 0.6 3 3 ­2 Yehudi 30 #NUM! #NUM! 0 12 #NUM! ­3 Tail 100 25 21.78 0.5 5 37 3.5 2414 Vertical 100 30 22.33 0.5 2 36 4 2 0 -2 0 0.6 2 4 6 8 10 12 13 3 -7 0 40 30 20 10 0 -10 -20 -30 -40 0 15 5 -5 -30 5 10 15 20 25 30 35 40 45 50 5 10 15 20 25 30 35 40 45 50 0.5 0.4 0.3 0.2 0.1 Top of climb ( 1g steady, l evel flight, M = 0.80 @ h=45K, service ceiling) Subsonic 2g manuever, 250kts @ h =10K T akeoff ground roll 4000 ft @ h = 5K, +15° hot day Landing ground roll 2500 ft @ h = 5K, +15° hot day Second segment climb gradient a bove h = 5K, +15° hot day W0/S & TSL/ W0 Value 0 50 60 70 80 90 100 110 120 130 -20 -10 0 10 20 30 Engine Unducted Fan Length Location x­location y­location z­location Thrust Performance Weight Number of Engine 2 38 3.5 7.5 3 40 0 7.5 4 4 43 0 7.5 2000 237 0 0 7.5 lbf lbs 2 0.5 0 7.5 4 47 47.5 Misson Sketch 45000 35000 25000 15000 5000 -5000 -500 Wind Flight Time diameter 2.09 4.5 2.09 0 50 ft/s 7.71 hrs 500 1000 1500 2000 2500 0 12 o f climb steady, el flight, M .80 @ 45K, sere ceiling) sonic 2g nuever, kts @ h 0K eoff und roll 0 ft @ h = +15° hot ding und roll 0 ft @ h = +15° hot o nd segnt climb dient ve h = 5K, 5° hot day /S & TSL/ Value Fuel Consumption Performance Area 2.662 ft^2 Diameter 2.089 ft Length 4.26 ft Volume 5.89 ft^3 Unducted Fan Number of Engine 1 Length 2 3 4 0 0.5 x­location 40 42 45 49 49.5 y­location 0 0 0 0 0 z­location 6.5 6.5 6.5 6.5 6.5 diameter ### 5 5 ### 4 Thrust #NUM! lbf Weight #NUM! lbs Area #NUM! ft^2 Diameter #NUM! ft Length #NUM! ft Volume #NUM! ft^3 Fuel Density Fuel Price Mission Fuel Price 6.8 4.42 #NUM! lb/Gal $/Gallon $ Location 1500 2000 2500 3000 3500 4000 4500 Length CenterLine Start diameter Volume Wetted Area 15 10 5 0 -5 -10 -15 0 10 5 0 -5 -10 10 5 0 -5 -30 0 Tail Yehudi Wing Area Sweep Angle Taper Ratio Aspect Ratio x­Location y­Location b/2 C1+C2 d C1 C2 C1quarter C2quarter 5 10 15 20 25 30 35 40 45 50 C1qLocation C2qLoaction Sweep angle angle Wetted Area sweep correction 5 10 15 20 25 30 35 40 45 50 Form Factor interference factor Mean Chord Length Center of Pressure Partial Lift -20 -10 0 10 20 30 Moment CenterLine Total Lift x y radius y­top y­bottom z­top z­bottom #NUM! 0 0 ­2 0 ­2 ­2 0 0 1 2.2 ­1.6 0.7 ­0.9 ­2.3 0.7 ­0.7 2 4.4 ­1.2 1.4 0.2 ­2.6 1.4 ­1.4 3 6.6 ­0.8 2.1 1.3 ­2.9 2.1 ­2.1 4 8.8 ­0.4 2.8 2.4 ­3.2 2.8 ­2.8 5 11 0 3.5 3.5 ­3.5 3.5 ­3.5 6 11 0 3.5 3.5 ­3.5 3.5 ­3.5 7 16.4 0 3.5 3.5 ­3.5 3.5 ­3.5 8 21.8 0 3.5 3.5 ­3.5 3.5 ­3.5 9 27.2 0 3.5 3.5 ­3.5 3.5 ­3.5 10 32.6 0 3.5 3.5 ­3.5 3.5 ­3.5 11 38 0 3.5 3.5 ­3.5 3.5 ­3.5 12 38 0 3.5 3.5 ­3.5 3.5 ­3.5 13 40.6 0.4 2.8 3.2 ­2.4 2.8 ­2.8 Canard Wing Fuselage mpannage E End 11 27 13 0 total length 51 x 0 11 38 51 diameter 7 y ­2 0 0 2 Fineness ratio 7.29 d 0 7 7 0 wetted area 922.6 141.11 ### 166.77 form factor 1.17 126.93 593.76 148.03 interference factor 1 0 Nose Fuselage Wing Fuselage Nose radius 0y ­2 0 Point # Angle y­position­position-1 z 0 0 0 ­2 -2 1 0.39 0 ­2 -3 2 0.79 0 ­2 0 3 1.18 0 ­2 4 1.57 0 ­2 5 1.96 0 ­2 6 2.36 0 ­2 7 2.75 0 ­2 8 3.14 0 ­2 9 3.53 0 ­2 10 3.93 0 ­2 11 4.32 0 ­2 12 4.71 0 ­2 13 5.11 0 ­2 14 5.5 0 ­2 15 5.89 0 ­2 16 6.28 0 ­2 radius 0.7 y ­1.6 0 Point # Angle y­position­position z -1 0 0 0 ­0.9 -2 1 0.39 0.27 ­0.95 -3 2 0.79 0.49 ­1.11 -1 3 1.18 0.65 ­1.33 4 1.57 0.7 ­1.6 5 1.96 0.65 ­1.87 6 2.36 0.49 ­2.09 7 2.75 0.27 ­2.25 8 3.14 0 ­2.3 9 3.53 ­0.27 ­2.25 10 3.93 ­0.49 ­2.09 11 4.32 ­0.65 ­1.87 12 4.71 ­0.7 ­1.6 13 5.11 ­0.65 ­1.33 14 5.5 ­0.49 ­1.11 15 5.89 ­0.27 ­0.95 16 6.28 0 ­0.9 radius 1.4 y ­1.2 2 0 -2 -4 -2 0.5 1 Section 0 Colu mn E 0 1 Section 1 Colum nE 0 2 Vertical Colum nE Tail 14 15 16 17 43.2 45.8 48.4 51 0.8 1.2 1.6 2 2.1 1.4 0.7 0 2.9 2.6 2.3 2 ­1.3 ­0.2 0.9 2 2.1 1.4 0.7 0 ­2.1 ­1.4 ­0.7 0 Tail Yehudi 2 Point # Angle y­position­position 0 z 0 0 0 0.2 -2 1 0.39 0.54 0.09 -4 2 0.79 0.99 ­0.21 -2 0 3 1.18 1.29 ­0.66 4 1.57 1.4 ­1.2 5 1.96 1.29 ­1.74 6 2.36 0.99 ­2.19 7 2.75 0.54 ­2.49 8 3.14 0 ­2.6 9 3.53 ­0.54 ­2.49 10 3.93 ­0.99 ­2.19 11 4.32 ­1.29 ­1.74 12 4.71 ­1.4 ­1.2 13 5.11 ­1.29 ­0.66 14 5.5 ­0.99 ­0.21 15 5.89 ­0.54 0.09 16 6.28 0 0.2 radius 2.1 y ­0.8 2 Point # Angle y­position­position 0 z 0 0 0 1.3 -2 1 0.39 0.8 1.14 -4 2 0.79 1.48 0.68 -5 0 3 1.18 1.94 0 4 1.57 2.1 ­0.8 5 1.96 1.94 ­1.6 6 2.36 1.48 ­2.28 7 2.75 0.8 ­2.74 8 3.14 0 ­2.9 9 3.53 ­0.8 ­2.74 10 3.93 ­1.48 ­2.28 11 4.32 ­1.94 ­1.6 12 4.71 ­2.1 ­0.8 13 5.11 ­1.94 0 14 5.5 ­1.48 0.68 15 5.89 ­0.8 1.14 16 6.28 0 1.3 radius 2.8 y ­0.4 5 Point # Angle y­position­position z 0 0 0 0 2.4 1 0.39 1.07 2.19 -5 2 0.79 1.98 1.58 -4 -2 0 3 1.18 2.59 0.67 4 1.57 2.8 ­0.4 5 1.96 2.59 ­1.47 Colum nE 2 Section 2 Colu mn E 5 Section 3 Colu mn E 2 4 Section 4 6 2.36 1.98 ­2.38 7 2.75 1.07 ­2.99 8 3.14 0 ­3.2 9 3.53 ­1.07 ­2.99 10 3.93 ­1.98 ­2.38 11 4.32 ­2.59 ­1.47 12 4.71 ­2.8 ­0.4 13 5.11 ­2.59 0.67 14 5.5 ­1.98 1.58 15 5.89 ­1.07 2.19 16 6.28 0 2.4 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 Section 4 Colu mn E 2 4 Section 5 Colu mn E 2 4 Section 6 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 2 4 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 2 4 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 -5 -4 -2 0 2 4 Colu mn E Section 7 Colum nE Section 8 Colu mn E 5 0 Colu mn E 2 4 Section 11 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 Section 9 Colu mn E 2 4 Section 10 Colu mn E 2 4 Section 11 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 3.5 y 05 Point # Angle y­position­position z 0 0 0 3.5 0 1 0.39 1.34 3.23 -5 2 0.79 2.47 2.47 -4 -2 0 3 1.18 3.23 1.34 4 1.57 3.5 0 5 1.96 3.23 ­1.34 6 2.36 2.47 ­2.47 7 2.75 1.34 ­3.23 8 3.14 0 ­3.5 9 3.53 ­1.34 ­3.23 10 3.93 ­2.47 ­2.47 11 4.32 ­3.23 ­1.34 12 4.71 ­3.5 0 13 5.11 ­3.23 1.34 14 5.5 ­2.47 2.47 15 5.89 ­1.34 3.23 16 6.28 0 3.5 radius 2.8 y 0.4 5 Point # Angle y­position­position z 0 0 0 3.2 0 1 0.39 1.07 2.99 -5 2 0.79 1.98 2.38 -4 -2 0 3 1.18 2.59 1.47 4 1.57 2.8 0.4 5 1.96 2.59 ­0.67 6 2.36 1.98 ­1.58 7 2.75 1.07 ­2.19 8 3.14 0 ­2.4 9 3.53 ­1.07 ­2.19 10 3.93 ­1.98 ­1.58 11 4.32 ­2.59 ­0.67 12 4.71 ­2.8 0.4 13 5.11 ­2.59 1.47 14 5.5 ­1.98 2.38 Colu mn E 2 4 Section 12 Colu mn E 2 4 Section 13 15 5.89 ­1.07 2.99 16 6.28 0 3.2 radius 2.1 y 0.8 4 Point # Angle y­position­position 2 z 0 0 0 2.9 0 1 0.39 0.8 2.74 -2 2 0.79 1.48 2.28 -5 3 1.18 1.94 1.6 4 1.57 2.1 0.8 5 1.96 1.94 0 6 2.36 1.48 ­0.68 7 2.75 0.8 ­1.14 8 3.14 0 ­1.3 9 3.53 ­0.8 ­1.14 10 3.93 ­1.48 ­0.68 11 4.32 ­1.94 0 12 4.71 ­2.1 0.8 13 5.11 ­1.94 1.6 14 5.5 ­1.48 2.28 15 5.89 ­0.8 2.74 16 6.28 0 2.9 radius 1.4 y 1.2 4 Point # Angle y­position­position 2 z 0 0 0 2.6 0 1 0.39 0.54 2.49 -2 2 0.79 0.99 2.19 -2 3 1.18 1.29 1.74 4 1.57 1.4 1.2 5 1.96 1.29 0.66 6 2.36 0.99 0.21 7 2.75 0.54 ­0.09 8 3.14 0 ­0.2 9 3.53 ­0.54 ­0.09 10 3.93 ­0.99 0.21 11 4.32 ­1.29 0.66 12 4.71 ­1.4 1.2 13 5.11 ­1.29 1.74 14 5.5 ­0.99 2.19 15 5.89 ­0.54 2.49 16 6.28 0 2.6 radius 0.7 y 1.6 3 Point # Angle y­position­position z 2 0 0 0 2.3 1 1 0.39 0.27 2.25 0 2 0.79 0.49 2.09 -1 Colu mn E 0 5 Section 14 Colu mn E 0 2 Section 15 Colu mn E 0 1 16 2 1 0 -1 0 1 Colu mn E 3 1.18 0.65 1.87 4 1.57 0.7 1.6 5 1.96 0.65 1.33 6 2.36 0.49 1.11 7 2.75 0.27 0.95 8 3.14 0 0.9 9 3.53 ­0.27 0.95 10 3.93 ­0.49 1.11 11 4.32 ­0.65 1.33 12 4.71 ­0.7 1.6 13 5.11 ­0.65 1.87 14 5.5 ­0.49 2.09 15 5.89 ­0.27 2.25 16 6.28 0 2.3 radius 0y 23 Point # Angle y­position­position z 2 0 0 0 21 1 0.39 0 2 0 2 0.79 0 20 3 1.18 0 2 4 1.57 0 2 5 1.96 0 2 6 2.36 0 2 7 2.75 0 2 8 3.14 0 2 9 3.53 0 2 10 3.93 0 2 11 4.32 0 2 12 4.71 0 2 13 5.11 0 2 14 5.5 0 2 15 5.89 0 2 16 6.28 0 2 Section 16 Colu mn E 0.5 1 Section 17 Wing Canard Yehudi Tail Vertical #NUM! 0 30 100 100 30 25 #NUM! 25 30 0.5 0.6 0 0.5 0.5 7.8 3 12 5 2 22 3 #NUM! 37 36 ­3 ­2 ­3 3.5 0 #NUM! 0 9.49 11.18 7.07 #NUM! #DIV/0! 3.16 8.94 14.14 #NUM! 0 #NUM! 5.21 4.08 #NUM! #DIV/0! 3.16 5.96 9.43 #NUM! #DIV/0! 0 2.98 4.71 #NUM! #DIV/0! 0.79 1.49 2.36 #NUM! #DIV/0! 0 0.75 1.18 #NUM! #DIV/0! #NUM! 38.49 38.36 #NUM! #DIV/0! #NUM! 42.96 41.26 #NUM! #DIV/0! #NUM! 21.78 22.33 #NUM! #NUM! 0 61.2 204 204 #NUM! #DIV/0! #NUM! 1.89 1.87 #NUM! #NUM! #NUM! #NUM! #NUM! 1 1 1 1 1 #NUM! #DIV/0! 1.58 4.47 7.07 #NUM! #DIV/0! #NUM! 40.72 39.81 #NUM! #NUM! #NUM! #NUM! #NUM! 0 #NUM! #NUM! Total Lift Total Moment AeroDynamic Center #NUM! #NUM! #NUM! x y z neg­z Wing Engines Unducted Fan Number of Engine 1 Length Engine 2 3 2 3 4 x 38 40 43 y 3.5 3.5 3.5 CenterLine z 7.5 7.5 7.5 diameter d 2.09 4 4.5 Wetted Area 13.13 37.7 56.55 Form Factor interference factor Jet Number of Engine x y CenterLine z diameter d Wetted Area Length 2 3 4 40 42 45 0 0 0 0 0 0 ### 5 5 ### 58.9 78.54 1 2 3 Engine 10 5 0 -5 20 20 10 0 -10 -20 0 8 6 4 2 0 -10 -8 25 30 35 40 45 50 55 A B C D A B C D A B x 22 #NUM! #NUM! #NUM! 3 3 #DIV/0! #DIV/0! #NUM! #NUM! y ­3 ­3 ­3 ­3 ­2 ­2 ­2 ­2 ­3 ­3 z 0 #NUM! #NUM! 0 x y z 0 #NUM! #NUM! 0 neg­z 0 0 0 0 0 0 0 0 neg­z 0 0 9.49 ­9.49 5 10 15 20 25 30 35 40 45 50 -6 -4 -2 0 2 4 6 8 10 C D A B C D A B C D x #NUM! #NUM! 37 42.21 45.19 42.96 36 40.08 44.8 45.43 y ­3 ­3 3.5 3.5 3.5 3.5 0 7.07 7.07 0 z x y z ­9.49 0 neg­z x y 0 0 38 11.18 ­11.18 38 11.18 ­11.18 40 0 0 43 47 0 47 0 38 0 38 0 40 43 47 47 radius Point # 9.49 0 z radius y­top y­bottom 3.5 ### 0 3.5 3.5 3.5 ### 1.04 4.54 2.46 3.5 ### 2 5.5 1.5 3.5 ### 2.25 5.75 1.25 3.5 ### 1.04 4.54 2.46 3.5 ### 0 3.5 3.5 3.5 ### 0 3.5 3.5 3.5 ### 1.04 4.54 2.46 3.5 ### 2 5.5 1.5 3.5 ### 2.25 5.75 1.25 3.5 ### 1.04 4.54 2.46 3.5 ### 0 3.5 3.5 ### x y z Angle x­position y­position z­position 00 38 3.5 8.54 1 ### 38 3.9 8.47 2 ### 38 4.24 8.24 3 ### 38 4.47 7.9 4 ### 38 4.54 7.5 5 ### 38 4.47 7.1 6 ### 38 4.24 6.76 7 ### 38 3.9 6.53 8 ### 38 3.5 6.46 9 ### 38 3.1 6.53 10 ### 38 2.76 6.76 11 ### 38 2.53 7.1 12 ### 38 2.46 7.5 13 ### 38 2.53 7.9 14 ### 38 2.76 8.24 15 ### 38 3.1 8.47 16 ### 38 3.5 8.54 2 Angle 00 40 3.5 9.5 1 ### 40 4.27 9.35 2 ### 40 4.91 8.91 3 ### 40 5.35 8.27 4 ### 40 5.5 7.5 5 ### 40 5.35 6.73 6 ### 40 4.91 6.09 Section 1 radius Point # Section 2 Section 2 radius Point # radius Point # 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 14 ### 15 ### 16 ### ### Angle 00 1 ### 2 ### 3 ### 4 ### 5 ### 6 ### 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 14 ### 15 ### 16 ### ### Angle 00 1 ### 2 ### 3 ### 4 ### 5 ### 6 ### 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 40 40 40 40 40 40 40 40 40 40 4.27 3.5 2.73 2.09 1.65 1.5 1.65 2.09 2.73 3.5 5.65 5.5 5.65 6.09 6.73 7.5 8.27 8.91 9.35 9.5 43 43 43 43 43 43 43 43 43 43 43 43 43 43 43 43 43 3.5 4.36 5.09 5.58 5.75 5.58 5.09 4.36 3.5 2.64 1.91 1.42 1.25 1.42 1.91 2.64 3.5 9.75 9.58 9.09 8.36 7.5 6.64 5.91 5.42 5.25 5.42 5.91 6.64 7.5 8.36 9.09 9.58 9.75 Section 3 47 47 47 47 47 47 47 47 47 47 47 47 47 47 3.5 3.9 4.24 4.47 4.54 4.47 4.24 3.9 3.5 3.1 2.76 2.53 2.46 2.53 8.54 8.47 8.24 7.9 7.5 7.1 6.76 6.53 6.46 6.53 6.76 7.1 7.5 7.9 Section 4 radius Point # 14 ### 47 2.76 8.24 15 ### 47 3.1 8.47 16 ### 47 3.5 8.54 0 Angle 00 0 0 0 1 ### 0 0 0 2 ### 0 0 0 3 ### 0 0 0 4 ### 0 0 0 5 ### 0 0 0 6 ### 0 0 0 7 ### 0 0 0 8 ### 0 0 0 9 ### 0 0 0 10 ### 0 0 0 11 ### 0 0 0 12 ### 0 0 0 13 ### 0 0 0 14 ### 0 0 0 15 ### 0 0 0 16 ### 0 0 0 z radius y­top y­bottom 00 0 0 0 0 0 ### ### ### 00 2.5 2.5 ­2.5 00 2.5 2.5 ­2.5 0 0 ### ### ### 00 0 0 0 ### x y z Angle x­position y­position z­position 00 40 ### ### 1 ### 40 ### ### 2 ### 40 ### ### 3 ### 40 ### ### 4 ### 40 ### ### 5 ### 40 ### ### 6 ### 40 ### ### 7 ### 40 ### ### 8 ### 40 ### ### 9 ### 40 ### ### 10 ### 40 ### ### 11 ### 40 ### ### x Prop 40 40 42 45 49 49 y radius Point # Section 1 Se radius Point # radius Point # radius Point # 12 ### 13 ### 14 ### 15 ### 16 ### ### Angle 00 1 ### 2 ### 3 ### 4 ### 5 ### 6 ### 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 14 ### 15 ### 16 ### ### Angle 00 1 ### 2 ### 3 ### 4 ### 5 ### 6 ### 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 14 ### 15 ### 16 ### ### Angle 40 40 40 40 40 ### ### ### ### ### ### ### ### ### ### 42 42 42 42 42 42 42 42 42 42 42 42 42 42 42 42 42 3.5 4.27 4.91 5.35 5.5 5.35 4.91 4.27 3.5 2.73 2.09 1.65 1.5 1.65 2.09 2.73 3.5 2.5 2.31 1.77 0.96 0 ­0.96 ­1.77 ­2.31 ­2.5 ­2.31 ­1.77 ­0.96 0 0.96 1.77 2.31 2.5 Section 2 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 45 3.5 4.36 5.09 5.58 5.75 5.58 5.09 4.36 3.5 2.64 1.91 1.42 1.25 1.42 1.91 2.64 3.5 2.5 2.31 1.77 0.96 0 ­0.96 ­1.77 ­2.31 ­2.5 ­2.31 ­1.77 ­0.96 0 0.96 1.77 2.31 2.5 Section 3 00 1 ### 2 ### 3 ### 4 ### 5 ### 6 ### 7 ### 8 ### 9 ### 10 ### 11 ### 12 ### 13 ### 14 ### 15 ### 16 ### 49 49 49 49 49 49 49 49 49 49 49 49 49 49 49 49 49 ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### ### Section 4 s 2 4 0 47 3.5 7.5 2.09 total r ctor 0 49 0 0 ### total 4 1 wetted area interference factor Skin Friction Coefficient Reynolds Number Coefficient Parasite Drag Fuselage 1.17 922.6 1 1.10E+08 0.002099 #NUM! Wing #NUM! #NUM! 1 #NUM! #NUM! #NUM! Canard #NUM! 0 1 #DIV/0! 0.000000 0.000000 Yehudi #NUM! 61.2 1 ### 0.003587 #NUM! Horizontal Tail #NUM! 204 1 9.69E+06 0.003019 #NUM! Vertical Tail #NUM! 204 1 1.53E+07 0.002808 #NUM! Nacelles 1.16 0 1 1.95E+07 0.002705 #NUM! 1.16 total #NUM! 1 Flight Conditions Atmosphere V 705.61 Viscosity 2.51E­07 h 42000 Re/l 2.17E+06 rho 0q 191.69 a 882.01 Coefficient of Lift Coefficient of Induced Drag ### Sum of CD Drag t/c MDD Mcr L/D #NUM! #NUM! #NUM! #NUM! lb #NUM! #NUM! #NUM! #NUM! form factor Drag 40 45 50 55 30 35 40 45 50 2 4 6 8 10 z­top z­bottom 7.5 7.5 8.54 6.46 9.5 5.5 9.75 5.25 8.54 6.46 7.5 7.5 ­7.5 ­7.5 ­8.54 ­6.46 ­9.5 ­5.5 ­9.75 ­5.25 ­8.54 ­6.46 ­7.5 ­7.5 neg­z ­8.54 ­8.47 ­8.24 ­7.9 ­7.5 ­7.1 ­6.76 ­6.53 ­6.46 ­6.53 ­6.76 ­7.1 ­7.5 ­7.9 ­8.24 ­8.47 ­8.54 ­9.5 ­9.35 ­8.91 ­8.27 ­7.5 ­6.73 ­6.09 ­5.65 ­5.5 ­5.65 ­6.09 ­6.73 ­7.5 ­8.27 ­8.91 ­9.35 ­9.5 ­9.75 ­9.58 ­9.09 ­8.36 ­7.5 ­6.64 ­5.91 ­5.42 ­5.25 ­5.42 ­5.91 ­6.64 ­7.5 ­8.36 ­9.09 ­9.58 ­9.75 ­8.54 ­8.47 ­8.24 ­7.9 ­7.5 ­7.1 ­6.76 ­6.53 ­6.46 ­6.53 ­6.76 ­7.1 ­7.5 ­7.9 ­8.24 ­8.47 ­8.54 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 z­top z­bottom 0 0 ### ### 2.5 ­2.5 2.5 ­2.5 ### ### 0 0 z­position Parasite Drag 435.543245 #NUM! 0.000000 #NUM! #NUM! #NUM! 0.000000 #NUM! Top of climb (1g steady, level flight, M = 0.80 @ h=45K, service ceiling) ρ α β M V CD0 AR e K CDC q n dh/dt g dV/dt 0 sl/ft^3 0.19 0.9496 0.8 774.48 ft/s 0.02 7.8 0.8 0.05 0 137.66 lb/ft^2 1 1.67 ft/s 32.17 ft/s^2 0 ft/s^2 ρ α Subsonic 2g manuever, 250kts @ h =10K 0 sl/ft^3 0.74 0.95 422 ft/s 0.02 7.8 0.8 156.36 lb/ft^2 2 0 ft/s 32.17 ft/s^2 0 ft/s^2 Second segment climb Takeoff ground roll 4000 ft @ Landing ground roll 2500 ft @ gradient above h = 5K, +15° h = 5K, +15° hot day h = 5K, +15° hot day hot day rho alpha beta CL max TO g s_to 0 sl/ft^3 0.84 1 1.6 32.17 ft/s^2 4000 ft rho alpha 0 sl/ft^3 0.95 rho alpha beta CL max TO g N CGR CD0 AR e_TO D CD0 β V CD0 AR e q n dh/dt g dV/dt 0.4 alpha_rev beta 1 1.6 CL max land g 32.17 ft/s^2 mu 0.3 2600 ft s_l Top of climb (1g steady, level flight, M = 0.80 @ h=45K, service ceiling) Exponential Regression for Top of climb (1g steady, level flight, M = 0.80 @ h=45K, service ceiling) Subsonic 2g manuever, 250kts @ h =10K Exponential Regression for Subsonic 2g manuever, 250kts @ h =10K Takeoff ground roll 4000 ft @ h = 5K, +15° hot day Linear Regression for Takeoff ground roll 4000 ft @ h = 5K, +15° hot day Exponential Regression for Takeoff ground roll 4000 ft @ h = 5K, +15° hot day Landing ground roll 2500 ft @ h = 5K, +15° hot day Linear Regression for Landing ground roll 2500 ft @ h = 5K, +15° hot day Linear Regression for Landing ground roll 2500 ft @ h = 5K, +15° hot day Second segment climb gradient above h = 5K, +15° hot day 0.3 Exponential Regression for Takeoff ground roll 4000 ft @ h = 5K, +15° hot day W0/S 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 TSL/W0 0.34 0.34 0.33 0.33 0.33 0.33 0.32 0.32 0.32 0.32 0.32 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.3 W0/S 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 TSL/W0 CL check W0/S 0.14 0.61 0.14 0.62 0.14 0.63 0.14 0.64 0.14 0.66 0.14 0.67 0.15 0.68 0.15 0.69 0.15 0.7 0.15 0.72 0.15 0.73 0.15 0.74 0.15 0.75 0.15 0.77 0.15 0.78 0.15 0.79 0.15 0.8 0.15 0.81 0.15 0.83 0.16 0.84 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 TSL/W0 0.18 0.18 0.18 0.19 0.19 0.19 0.2 0.2 0.2 0.21 0.21 0.22 0.22 0.22 0.23 0.23 0.23 0.24 0.24 0.24 W0/S 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 TSL/W0 ­0.21 ­0.2 ­0.19 ­0.18 ­0.17 ­0.16 ­0.14 ­0.13 ­0.12 ­0.11 ­0.1 ­0.09 ­0.08 ­0.06 ­0.05 ­0.04 ­0.03 ­0.02 ­0.01 0 W0/S 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.3 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.32 0.32 0.32 0.32 0.32 0.32 0.32 0.32 0.32 0.32 0.32 0.33 0.33 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.17 0.17 0.17 0.17 0.17 0.17 0.17 0.17 0.17 0.18 0.18 0.18 0.18 0.18 0.18 0.18 0.18 0.19 0.19 0.19 0.19 0.19 0.19 0.19 0.19 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.2 0.21 0.21 0.21 0.21 0.21 0.21 0.21 0.22 0.22 0.22 0.22 0.22 0.22 0.22 0.23 0.23 0.23 0.23 0.85 0.86 0.87 0.89 0.9 0.91 0.92 0.94 0.95 0.96 0.97 0.98 1 1.01 1.02 1.03 1.05 1.06 1.07 1.08 1.09 1.11 1.12 1.13 1.14 1.15 1.17 1.18 1.19 1.2 1.22 1.23 1.24 1.25 1.26 1.28 1.29 1.3 1.31 1.32 1.34 1.35 1.36 1.37 1.39 1.4 1.41 1.42 1.43 1.45 1.46 1.47 1.48 1.49 1.51 1.52 1.53 1.54 1.56 1.57 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 0.25 0.25 0.25 0.26 0.26 0.26 0.27 0.27 0.28 0.28 0.28 0.29 0.29 0.29 0.3 0.3 0.3 0.31 0.31 0.31 0.32 0.32 0.32 0.33 0.33 0.34 0.34 0.34 0.35 0.35 0.35 0.36 0.36 0.36 0.37 0.37 0.37 0.38 0.38 0.38 0.39 0.39 0.4 0.4 0.4 0.41 0.41 0.41 0.42 0.42 0.42 0.43 0.43 0.43 0.44 0.44 0.44 0.45 0.45 0.46 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.1 0.11 0.12 0.13 0.14 0.15 0.16 0.18 0.19 0.2 0.21 0.22 0.23 0.25 0.26 0.27 0.28 0.29 0.3 0.31 0.33 0.34 0.35 0.36 0.37 0.38 0.39 0.41 0.42 0.43 0.44 0.45 0.46 0.47 0.49 0.5 0.51 0.52 0.53 0.54 0.55 0.57 0.58 0.59 0.6 0.61 0.62 0.63 0.65 0.66 0.67 0.68 0.69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 0.33 0.33 0.33 0.33 0.33 0.33 0.33 0.34 0.34 0.34 0.34 0.34 0.34 0.34 0.34 0.34 0.35 0.35 0.35 0.35 0.35 12 0.2 0.19 0.19 0.19 0.18 0.18 0.18 0.17 0.17 0.17 0.17 0.17 0.16 0.16 0.16 0.16 0.15 0.15 0.15 0.15 0.15 0.15 0.14 0.14 0.14 0.14 0.14 0.14 0.14 0.13 0.13 0.13 0.13 0.13 0.13 0.13 0.13 0.12 13 0.27 0.28 0.3 0.31 0.33 0.34 0.36 0.37 0.39 0.4 0.41 0.43 0.44 0.45 0.47 0.48 0.49 0.51 0.52 0.53 0.55 0.56 0.57 0.59 0.6 0.61 0.62 0.64 0.65 0.66 0.67 0.68 0.7 0.71 0.72 0.73 0.75 0.76 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 14 49.66 50.66 51.67 52.67 53.67 54.67 55.68 56.68 57.68 58.68 59.68 60.69 61.69 62.69 63.69 64.69 65.69 66.69 67.69 68.7 69.7 70.7 71.7 72.7 73.7 74.7 75.7 76.7 77.7 78.7 79.7 80.7 81.7 82.7 83.7 84.7 85.7 86.7 0.23 0.23 0.23 0.24 0.24 0.24 0.24 0.24 0.24 0.24 0.25 0.25 0.25 0.25 0.25 0.25 0.25 0.26 0.26 0.26 0.26 15 0.16 0.16 0.15 0.14 0.14 0.13 0.13 0.12 0.11 0.11 0.1 0.1 0.09 0.09 0.08 0.08 0.07 0.07 0.07 0.06 0.06 0.05 0.05 0.04 0.04 0.04 0.03 0.03 0.02 0.02 0.02 0.01 0.01 0.01 0 0 0 0.01 1.58 1.59 1.6 1.62 1.63 1.64 1.65 1.66 1.68 1.69 1.7 1.71 1.73 1.74 1.75 1.76 1.77 1.79 1.8 1.81 1.82 23 0.03 0.04 0.04 0.04 0.05 0.05 0.05 0.05 0.06 0.06 0.06 0.07 0.07 0.07 0.07 0.08 0.08 0.08 0.09 0.09 0.09 0.09 0.1 0.1 0.1 0.1 0.11 0.11 0.11 0.11 0.12 0.12 0.12 0.12 0.13 0.13 0.13 0.13 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 24 0.36 0.34 0.33 0.32 0.31 0.3 0.29 0.28 0.27 0.26 0.25 0.24 0.23 0.21 0.2 0.19 0.18 0.17 0.16 0.15 0.14 0.13 0.12 0.11 0.1 0.09 0.08 0.07 0.06 0.05 0.04 0.03 0.02 0.01 0.01 0.02 0.03 0.04 0.46 0.46 0.47 0.47 0.47 0.48 0.48 0.48 0.49 0.49 0.49 0.5 0.5 0.5 0.51 0.51 0.52 0.52 0.52 0.53 0.53 25 0.17 0.17 0.17 0.17 0.17 0.17 0.17 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.16 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.14 0.14 0.14 0.14 0.14 0.14 0.14 0.14 34 0.39 0.38 0.37 0.37 0.36 0.35 0.34 0.33 0.33 0.32 0.31 0.3 0.29 0.29 0.28 0.27 0.26 0.25 0.25 0.24 0.23 0.22 0.22 0.21 0.2 0.19 0.18 0.18 0.17 0.16 0.15 0.14 0.14 0.13 0.12 0.11 0.1 0.1 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 35 0.13 0.13 0.13 0.12 0.12 0.12 0.11 0.11 0.11 0.1 0.1 0.1 0.09 0.09 0.09 0.08 0.08 0.07 0.07 0.07 0.06 0.06 0.06 0.05 0.05 0.05 0.04 0.04 0.04 0.03 0.03 0.03 0.02 0.02 0.01 0.01 0.01 0 0.7 0.72 0.73 0.74 0.75 0.76 0.77 0.78 0.8 0.81 0.82 0.83 0.84 0.85 0.86 0.88 0.89 0.9 0.91 0.92 0.93 45 0.52 0.51 0.5 0.49 0.48 0.47 0.46 0.44 0.43 0.42 0.41 0.4 0.39 0.38 0.36 0.35 0.34 0.33 0.32 0.31 0.3 0.28 0.27 0.26 0.25 0.24 0.23 0.21 0.2 0.19 0.18 0.17 0.16 0.15 0.13 0.12 0.11 0.1 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 Max 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.77 0.78 0.79 0.81 0.82 0.83 0.84 0.85 0.86 0.88 0.89 0.9 0.91 0.92 0.93 0.95 0.96 0.97 0.98 0.99 1 1.02 1.03 1.04 1.05 1.06 1.07 1.08 1.09 1.11 1.12 1.13 1.14 1.15 1.16 1.17 1.18 1.2 1.21 1.22 1.23 1.24 1.25 1.26 1.27 1.29 1.3 1.31 1.32 1.33 1.34 1.35 1.36 1.37 1.38 1.4 1.41 1.42 1.43 1.44 87.7 88.7 89.7 90.7 91.7 92.7 93.7 94.7 95.7 96.7 97.7 98.7 99.7 100.7 101.69 102.69 103.69 104.69 105.69 106.69 107.69 108.69 109.69 110.69 111.69 112.69 113.69 114.69 115.69 116.68 117.68 118.68 119.68 120.68 121.68 122.68 123.68 124.68 125.68 126.68 127.67 128.67 129.67 130.67 131.67 132.67 133.67 134.67 135.67 136.66 137.66 138.66 139.66 140.66 141.66 142.66 143.66 144.66 145.65 146.65 0.01 0.01 0.02 0.02 0.02 0.03 0.03 0.03 0.04 0.04 0.04 0.05 0.05 0.05 0.05 0.06 0.06 0.06 0.07 0.07 0.07 0.08 0.08 0.08 0.08 0.09 0.09 0.09 0.09 0.1 0.1 0.1 0.11 0.11 0.11 0.11 0.12 0.12 0.12 0.12 0.13 0.13 0.13 0.13 0.14 0.14 0.14 0.14 0.15 0.15 0.15 0.15 0.16 0.16 0.16 0.16 0.17 0.17 0.17 0.17 0.13 0.14 0.14 0.14 0.14 0.15 0.15 0.15 0.15 0.16 0.16 0.16 0.16 0.16 0.17 0.17 0.17 0.17 0.18 0.18 0.18 0.18 0.18 0.19 0.19 0.19 0.19 0.2 0.2 0.2 0.2 0.2 0.21 0.21 0.21 0.21 0.21 0.22 0.22 0.22 0.22 0.23 0.23 0.23 0.23 0.23 0.24 0.24 0.24 0.24 0.24 0.25 0.25 0.25 0.25 0.26 0.26 0.26 0.26 0.26 0.05 0.06 0.07 0.08 0.09 0.1 0.11 0.12 0.13 0.14 0.15 0.16 0.17 0.18 0.19 0.2 0.21 0.22 0.23 0.24 0.25 0.26 0.27 0.28 0.29 0.3 0.31 0.32 0.33 0.34 0.35 0.36 0.37 0.38 0.39 0.4 0.41 0.42 0.43 0.44 0.45 0.46 0.47 0.48 0.49 0.5 0.51 0.52 0.53 0.54 0.55 0.56 0.57 0.58 0.59 0.6 0.61 0.62 0.63 0.64 0.14 0.13 0.13 0.13 0.13 0.13 0.13 0.13 0.13 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.12 0.11 0.11 0.11 0.11 0.11 0.11 0.11 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.09 0.09 0.09 0.09 0.09 0.09 0.09 0.08 0.08 0.08 0.08 0.08 0.08 0.08 0.07 0.07 0.07 0.07 0.07 0.07 0.07 0.06 0.06 0.06 0.06 0.06 0.06 0.06 0.09 0.08 0.07 0.06 0.06 0.05 0.04 0.03 0.02 0.02 0.01 0 0.01 0.02 0.02 0.03 0.04 0.05 0.05 0.06 0.07 0.08 0.09 0.09 0.1 0.11 0.12 0.13 0.13 0.14 0.15 0.16 0.17 0.17 0.18 0.19 0.2 0.21 0.21 0.22 0.23 0.24 0.25 0.25 0.26 0.27 0.28 0.28 0.29 0.3 0.31 0.32 0.32 0.33 0.34 0.35 0.36 0.36 0.37 0.38 0 0 0.01 0.01 0.01 0.02 0.02 0.02 0.03 0.03 0.03 0.04 0.04 0.05 0.05 0.05 0.06 0.06 0.06 0.07 0.07 0.07 0.08 0.08 0.08 0.09 0.09 0.09 0.1 0.1 0.11 0.11 0.11 0.12 0.12 0.12 0.13 0.13 0.13 0.14 0.14 0.14 0.15 0.15 0.15 0.16 0.16 0.17 0.17 0.17 0.18 0.18 0.18 0.19 0.19 0.19 0.2 0.2 0.2 0.21 0.09 0.08 0.07 0.05 0.04 0.03 0.02 0.01 0 0.01 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.11 0.12 0.13 0.14 0.15 0.16 0.17 0.19 0.2 0.21 0.22 0.23 0.24 0.26 0.27 0.28 0.29 0.3 0.31 0.32 0.34 0.35 0.36 0.37 0.38 0.39 0.4 0.42 0.43 0.44 0.45 0.46 0.47 0.48 0.5 0.51 0.52 0.53 0.54 0.55 0.56 0.58 0.59 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 min 0.09 0.09 0.09 0 1.45 1.46 1.47 0 147.65 148.65 149.65 0 0.17 0.18 0.18 0 0.27 0.27 0.27 0 0.65 0.66 0.67 0.01 0.05 0.05 0.05 0 0.39 0.4 0.4 0 0.21 0.21 0.22 0 0.6 0.61 0.62 0 148 149 150 Max max2 First Point x y Second segment climb gradient above h = 5K, +15° hot day 0 0.84 1 1.5 32.17 ft/s^2 2 2.4 % 0 7.8 0.6 0 W0/S TSL/W0 W0/S & TSL/W0 Value Average Fudge Factor Included 11 W0/S 0.33 TSL/W0 70 0.3 984.87 Regression for ground roll @ h = 5K, ot day Regression for ground roll @ h = 5K, ot day segment radient above , +15° hot day 0.3 1239.55 TSL/W0 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 y 5000 ft rho = p= R= T= 0 sl/ft3 1760.9 lb/ft2 1718 ft-lb/sl-ºR 500.86 ºR 5000 ft hot day (∆T = +15) 0 sl/ft3 1760.9 lb/ft2 1718 ft-lb/sl-ºR 515.86 ºR 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 0.31 12 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 13 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 14 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 15 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.3 0 0 23 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 24 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.17 0 0 0 0 25 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 34 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 35 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 45 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 12 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 13 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.35 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.31 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.31 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0.3 0.3 0 0 0 0 0 0 0 0 0.17 0.17 0 0 0 0 0 0 0 0 0.35 0 0 0 0 0.31 0.31 0 0 0 0.31 y 0.31 x x2 0 0 0 0 0 0 0 0 0 0 0 0 First Point 99 0.35 Second Point 96 0.31 Average x y 97.5 0.33 Fudge Factor Included 92.63 0.36 14 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 15 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 85 0 0 23 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 24 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 83 0 0 0 0 25 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 34 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 35 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 45 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 99 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 88 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 96 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 85 0 0 0 0 0 0 0 0 0 0 0 83 0 0 0 0 0 0 0 0 0 0 0 99 99 0 0 0 0 88 0 88 0 0 0 96 0 96 W0 guess #NUM! lb number of passengers 9 number of flight crew 2 We/W0 #NUM! empty weight fraction Wpayload 2160 lb Wcrew 480 lb W0 design #NUM! lb We design #NUM! lb Wf design #NUM! lb design mission range 3700 nmi alternate airport range 200 nmi reserve loiter 0.6 hr AR 7.8 T/W0 0.5 W0/S 110 lb/ft2 Mmax 0.820 subsonic (L/D)max 18.02 subsonic (L/D)cruise 15.68 subsonic (L/D)loiter 18.02 SFCcruise 0.5 1/hr Mcruise 0.800 Vcruise @ 42,000 ft 458.54 kts SFCloiter 0.4 1/hr design mission W1/W0 0.97 takeoff W2/W1 0.98 climb W3/W2 0.77310 cruise W4/W3 1 land W5/W4 0.97 missed approach (TO) W6/W5 0.98 climb W7/W6 0.98619 divert to alternate W8/W7 0.98677 hold W9/W8 1 land W9/W0 0.67169 Wf/W0 0.33160 fuel weight fraction Thrust #NUM! S #NUM! Initial Weight Prediction X­ # Location 1 #NUM! 1 40.72 1 39.81 1 44.5 1 #NUM! 1 11 1 43 1 43 1 43 1 #NUM! 1 11 1 43 1 11 1 #NUM! 1 #NUM! 1 7.33 2 #NUM! 2 40.72 2 #NUM! 2 #NUM! 1 43 2 #NUM! 1 20 1 16.7 Seat2 1 17.7 Seat3 1 25.46 Seat4 1 30.34 Seat5 1 15.63 Seat6 1 30.34 Sofa 1 21.65 Laboratory 1 33.9 Gally 1 13 Environmental Control 20 1 APU 1 43 Pilot 2 20 Passanger1 1 16.7 Passanger2 1 17.7 Passanger3 1 25.46 Passanger4 1 30.34 Passanger5 1 15.63 Passanger6 1 30.34 Passanger7 1 21.65 Name Wwing Whorizont Wverticalt altail Wfuselag ail Wmain e Wnose landing landing gear Wnacelle gear Wengine group Wstarter( controls pneumati Wfuel c) Wflight system Wapu controls Winstrum installed Wfurnishi Whydrauli ents ng(does Welectric cs not al Wavionics include Waircondi cargo tioning handling Wanti­ice Whandlin gear or Wcargo g gear seats) Wengine handling gear and Avionics seats Seat1 Center of Gravity Weight #NUM! #NUM! 0 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 234 195 195 195 195 195 195 195 Payload Inner Structure Outer Structure Passanger8 1 Passanger9 1 Luggage 2 Total 0 Payload 21.65 21.65 #NUM! #NUM! 195 195 234 #NUM! vity Moment From Zero #NUM! Point #NUM! 0 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­ #NUM! 30935.4 #NUM! 9 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 4680 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 Constants Constants A Bh Bw D De Fw Ht Ht/Hv Hv Iy Kcb Kdoor Kdw Kdwf Kh KLg Kmc Kmp Kng Knp Kp Kr Krht Ktp Ktpg Ktr Kuht Kvg Kvs Kvsh Kws Ky Kz L La Ld Lec Lf Lm Ln Lt Ltp Value Option 7.8 aspect ratio 22.36 horizontal tail span #NUM! wingspan 1.5 fuselage structural depth 2.09 engine diameter 7 fuselage width at horizontal tail intersection ft 3.5 horizontal tail height above fuselage ft 0 0 for conventional tail, 1 for "T" tail 4.27 vertical tail height above fuselage 2500 yawing moment of inertia lb­ft^2 1 2.25 for cross­beam gear, 1 otherwise 1 1 for no cargo door, 1.06 for on side cargo door, 1. 1 0.768 for delta wing 1 otherwise 1 0.774 for deltawing aircraft 1 otherwise 0.12 0.05 for low subsonic flight 0.11 for midium subsonic flight, 0.12 for high subso 1.12 1.12 for fuselage mounted 1 otherwise 1.45 1.45 if mission completiong required after failure 1 otherwise 1 1.126 for kneeling gear 1 otherwise 1.02 1.017 for pylon mounted nacelle 1 otherwise 1 1.15 for kneeling gear 1 otherwise 1 1.4 for engine with propeller 1 otherwise 1 1.133 if reciprocating engine 1 otherwise 1.05 1.047 for rolling horizontal tail otherwise 1 0.79 0.793 if turboprop 1 otherwise 1 0.826 for tripod gear 1 otherwise 1.18 1.18 for jet with thrust reversals 1 otherwise 1 1.143 for unit(all­moving) horizontal tail 1 otherwise 1 1.62 for variable geometry 1 otherwise 1 1.19 for variable sweep wing 1 otherwise 1 1.425 for variable sweep wing 1 otherwise 4.5 aircraft pitching radius of gyration (~=0.3Lt) 15 aircraft yawing radius of gyration (~=Lt) 48 Fuselage structural length(excludes radome cowling, tail cap) 38 Electrical routing distance(generators to avionics to cockpit) 2 Duct Length 38 length from engine front to cockpit 51 total fuselage length 60 extended length of main landing gear in 60 extended nose gear length in 15 tail length; wing quarter 1 length of tail pipe 4221.75 4221.75 #NUM! #NUM! M Nc Nci Nen Nf Ngen NLt Nl Nm Nmss Nmw Nnw Np Nt Nu Nw Nz Rkva Scs Scsw Se Sf Sht Sn Svt Sw SFC Vi Vp Vpr Vt Wc Wdg Wec Wen Wl Wuav Lamda lamda t/c Fw/Bh Lamdaht Ah Lamdavt Av 0.800 mach number 2 number of crew 2 number of crew equivalents 2 number of engines 5 number of functions performed by controls (4~7) 2 number of generators(typically Nen) 9 nacelle length ft 3 ultimate landing load factor ;=Ngear*1.5 1 number of mechanical functions (typically 0~2) 2 number of main gear shock struts 2 number of main wheels 1 number of nose wheels 11 number of personnel onboard (crew+passengers) 5 number of fuel tanks 7 number of hydraulic utiliity functions (typically 5~15) 4.5 nacelle width ft 5 ultimate load factor ;=1.5*limit load factor 50 system electrical rating kV*A (Typically 40~50 for transports) 70 total area of control surfaces ft^2 78 control surface area ft^2 20 elevator area ft^2 922.6 fuselage wetted area ft^2 100 horizontal tail area ft^2 0 nacelle wetted area ft^2 100 vertical tail area ft^2 #NUM! trapazoidal wing area ft^2 0.5 Engine Specific fuel consumption­­maximum thrust 2180 integral tanks volume gal 0 self­sealing tanks volume gal 935 volume of pressurized section ft^3 2180 total fuel volume gal 4000 maximum cargo weight lb #NUM! flight design gross weight lb 1836 weight of engine and contents lb 1364 engine weight, each lb 25000 landing design gross weight lb #NUM! uninstalled avionics weight lb (typically 800~1400 #NUM! wing sweep at 25% MAC 0.5 taper ratio #NUM! #NUM! 21.78 horizontal tail wing sweep 100 area of horizontal tail 22.33 Vertical tail wing sweep 100 area of vertical tail t/c vertical L/D Vstall 0.5 32 88.64 Detailed Weight Prediction W0 guess W0 design Wf design We/W0 #NUM! #NUM! #NUM! #NUM! #NUM! We Thrust #NUM! Wing Area #NUM! Wwing #NUM! Whorizontaltail #NUM! Wverticaltail #NUM! Wfuselage #NUM! Wmain landing gear 798.17 Wnose landing gear 214.15 Wnacelle group 0 Wengine controls 40.4 Wstarter(pneumatic) 84.66 Wfuel system 283.58 Wflight controls 456.01 Wapu installed 198 Winstruments #NUM! Whydraulics #NUM! Welectrical 586.26 Wavionics #NUM! Wfurnishing(does not include cargo handling gear or seats) 269.55 Wairconditioning #NUM! Wanti­ice #NUM! Whandling gear #NUM! Wengine #NUM! Wcargo handling gear and seats 700 #NUM! ome cowling, tail cap) o avionics to cockpit) load factor ically 40~50 for transports) imum thrust ly 800~1400 NACA number m (maximum chamber) p (location of maximum chamber) maximum thickness 2414 0.02 0.40 0.14 t 0.14 c #NUM! m 0.02 7 5 3 1 -1 -3 0 Section x 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! y 2 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! yc 4 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 6 8 10 12 xupper yupper xlower ylower #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! p 0.40 10 theta 12 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Mission Detail Misson Distance Altitude Acculative Distance Taxi Distance h R gamma T0 P0 rho0 Th_trop Th_stra h_trop h_stra g T1 P1 P2 T P rho a Ft to Miles Hour Mach Number Velocity Flgith Time Weight AC Cl Fuel FractionW1/W0 Weight of Fuel 4000 0 0 #DIV/0! #NUM! #NUM! 0.97 W2/W1 #NUM! #NUM! 0.0 #NUM! #DIV/0! 0.0 0.0 0.0 0.0 #NUM! #NUM! 230661995.4 #NUM! #DIV/0! 7151149.8 20226505.9 31980913.9 40705058.0 10560 #NUM! #NUM! 0.99 W3/W2 #NUM! #NUM! 101374689.0 #NUM! #DIV/0! 3142891.3 8889439.0 14055437.3 17889651.0 0.6 646.38 16.34 158400 #NUM! #NUM! 0.75 W4/W3 #NUM! #NUM! 110485797.1 #NUM! #DIV/0! 3425360.5 9688382.5 15318677.7 19497493.6 0.65 570.4 277.7 0.8 705.61 18214960 25814.44 0 #NUM! #NUM! 0.99 W5/W4 #NUM! #NUM! 92949033.8 #NUM! #DIV/0! 2881673.1 8150602.3 12887233.8 16402770.7 #NUM! #NUM! 4000 0h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 518.69 T 2116.2 P 0 rho 1116.29 a 0.76 Miles Initial 0 0 0 Taxi 0.76 0 0.76 Take off Distance 2 10000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 483.09 T 1454.76 P 0 rho 1077.3 a 2 Miles Takeoff 2 10000 2.76 Climb 30 40000 32.76 Climb Distance 30 40000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 320.54 T 480.74 P 0 rho 877.54 a 30 Miles Cruise 3449.8 42000 3482.56 Loiter Attept to Land 0 16000 3482.56 Cruise Distance 3449.8 42000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 323.82 T 427.88 P 0 rho 882.01 a 3449.8 Miles 0.5 0.3 315.96 0.95 2000 3483.51 Climb 16 10000 3499.51 Loiter Distance Total Weight Fuselage Wing Canard Yehudi Horizontal Tail Vertical Tail Nacelles Reynold's Fuselage Wing Canard Yehudi Horizontal Tail Vertical Tail Nacelles Skin Friction Err:502 #NUM! #DIV/0! Err:502 Err:502 Err:502 Err:502 0.00189811 #NUM! #DIV/0! 0.00317113 0.00268986 0.00250971 0.00242154 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00212427 #NUM! #DIV/0! 0.00364045 0.00306106 0.00284603 0.00274118 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00209889 #NUM! #DIV/0! 0.00358697 0.00301899 0.00280799 0.00270506 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00215028 #NUM! #DIV/0! 0.00369550 0.00310431 0.00288511 0.00277827 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Fuselage Err:502 Wing #NUM! Canard 0.00000000 Yehudi Err:502 Horizontal Tail Err:502 Vertical Tail Err:502 Nacelles Err:502 Total CD Parasite Err:502 Induced Drag Total CD Drag 50000 40000 30000 20000 10000 0 -10000 0 -500 -100 -200 -300 -400 -500 -600 -500 0 0 #NUM! Err:502 Err:502 Coefficient of P 500 1000 1500 2 500 1000 1500 20 Name Err:509 Err:509 Err:509 X­Location #NUM! 40.72 39.81 Take Off Gear up Fuselage Tank Wing Tank Moment Moment Moment Weight From Zero Weight From Zero Weight From Zero Weight #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Point Point Point #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0 0 0 0 0 0 0 Err:509 44.5 0 Err:509 #NUM! 798.17 Err:509 11 214.15 Err:509 43 0 Err:509 43 40.4 Err:509 43 84.66 Err:509 #NUM! 283.58 Err:509 11 456.01 Err:509 43 198 Err:509 11 #NUM! Err:509 #NUM! #NUM! Err:509 #NUM! 586.26 Err:509 7.33 #NUM! Err:509 #NUM! 269.55 Err:509 40.72 #NUM! Err:509 #NUM! 0 Err:509 #NUM! 0 Err:509 43 ­719.43 Err:509 #NUM! 700 Avionics 20 234 Seat1 16.7 34 Seat2 17.7 34 Seat3 25.46 34 Seat4 30.34 34 Seat5 15.63 34 Seat6 30.34 34 Sofa 21.65 34 Laboratory 33.9 34 Gally 13 34 Environmental Control 20 30 APU 43 90 Fuel Pilot Passanger1 Passanger2 Passanger3 Passanger4 Passanger5 Passanger6 Passanger7 Passanger8 Passanger9 Luggage 0 Take Off 20 16.7 17.7 25.46 30.34 15.63 30.34 21.65 21.65 21.65 #NUM! #NUM! #NUM! Gear up #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 0 #NUM! 798.17 2355.66 214.15 0 0 1737.2 40.4 3640.3 84.66 #NUM! 283.58 5016.16 456.01 8514 198 #NUM! #NUM! #NUM! #NUM! #NUM! 586.26 #NUM! #NUM! #NUM! 269.55 #NUM! #NUM! #NUM! 0 #NUM! 0 ­30935.49 ­719.43 #NUM! 700 4680 234 567.8 34 601.8 34 865.64 34 1031.39 34 531.42 34 1031.39 34 736.1 34 1152.6 34 442 34 600 30 3870 90 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! Total Payload Fuel Inner Structure Outer Structure Fuselage Tank Wing Tank Gear DownLand Reserve Fuel Passenger Off Crew Off CG Weight #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Divert 200 40000 3699.51 Loiter 0 16000 h 1716 R Loiter 0 16000 3699.51 Distance Land 0.49 2000 3700 Climb Distance 16 10000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 483.09 T 1454.76 P 0 rho 1077.3 a 16 Miles 0.65 700.25 9.02 84480 120.64 #NUM! #NUM! 0.99 W7/W6 0.98 W8/W7 #NUM! #NUM! 249883828.3 #NUM! #DIV/0! 7747078.9 21912048.1 34645990.1 44097146.2 #NUM! #NUM! 124768848.0 #NUM! #DIV/0! 3868173.9 10940848.1 17298999.7 22018032.0 1056000 0.8 702.03 1504.21 0 #NUM! #NUM! 0.99 W9/W8 #NUM! #NUM! 92949033.8 #NUM! #DIV/0! 2881673.1 8150602.3 12887233.8 16402770.7 1 W9/W0 #NUM! #NUM! 126314070.8 #NUM! #DIV/0! 3916080.0 11076347.0 17513242.4 22290718.4 #NUM! #NUM! Divert Distance 200 40000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 320.54 T 480.74 P 0 rho 877.54 a 200 Miles 0.3 0.3 315.96 0 2600 #NUM! #NUM! Loiter Distance 0 16000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 461.73 T 1146.22 P 0 rho 1053.21 a 0 Ft to Miles 0.25 277.15 Land Distance 5000 2000 h 1716 R 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 511.57 T 1967.51 P 0 rho 1108.6 a 0.95 Miles Attempt to Land 1.4 gamma 518.69 T0 2116.2 P0 0 rho0 0 Th_trop 0 Th_stra 36152 h_trop 82346 h_stra 32.2 g 389.99 T1 470.674 P1 50.98 P2 461.73 T 1146.22 P 0 rho 1053.21 a 0 Ft to Miles 0.5 0.3 315.96 0 #NUM! #NUM! 0.97 W6/W5 #NUM! #NUM! Reynold's number 92949033.8 #NUM! #DIV/0! 2881673.1 8150602.3 12887233.8 16402770.7 252628141.6 #NUM! #DIV/0! 7832160.1 22152694.0 35026484.7 44581436.8 #NUM! #NUM! 5000 #NUM! #NUM! 0.5 554.3 Skin Friction Coefficient 0.00215028 #NUM! #DIV/0! 0.00369550 0.00310431 0.00288511 0.00277827 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00187517 #NUM! #DIV/0! 0.00312446 0.00265270 0.00247594 0.00238940 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00187790 #NUM! #DIV/0! 0.00313001 0.00265712 0.00247996 0.00239323 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00206376 #NUM! #DIV/0! 0.00351327 0.00296091 0.00275545 0.00265516 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00215028 #NUM! #DIV/0! 0.00369550 0.00310431 0.00288511 0.00277827 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0.00206025 #NUM! #DIV/0! 0.00350592 0.00295512 0.00275020 0.00265018 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Coefficient of Parasite Drag 12 10 8 500 2000 2500 3000 3500 4000 6 4 2 0 00 2000 Wing Tank Gear Down Land Reserve Fuel Passenger Off Crew Off Moment Moment Moment Moment Moment From Zero Weight From Zero Weight From Zero Weight From Zero Weight From Zero Weight #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Point Point Point Point Point #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 0 0 0 0 0 0 0 0 0 0 CG Travel 2500 3000 3500 4000 0 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! Add Fuel 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 0 0 0 0 0 0 0 0 0 0 #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 0 0 0 0 0 0 0 0 0 0 0 #NUM! Add Crew Add Passenger #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! Land 2600 2000 1716 1.4 518.69 2116.2 0 0 0 36152 82346 32.2 389.99 470.674 50.98 511.57 1967.51 0 1108.6 0.49 0.25 277.15 9.38 #NUM! #NUM! 0.67 #NUM! #NUM! 126314070.8 #NUM! #DIV/0! 3916080.0 11076347.0 17513242.4 22290718.4 Wf/W0 0.35 Runway 1 x y Runway 2 x y #NUM! 0 1 100 0 1 3600 2000 #NUM! 0.76 2 0 ­5000 2 3700 ­3000 #NUM! 2.76 3 ­300 0 3 4000 2000 #NUM! 32.76 4 ­180 3000 4 3880 5000 #NUM! 3482.56 1 100 0 1 3600 2000 #NUM! 3482.56 #NUM! 3483.51 Drag Coeff. form factor Fuselage Wing Nacelles 1.17 #NUM! 1.16 wetted area interference factor 922.6 #NUM! 0 1 1 1 0.00206025 #NUM! #DIV/0! 0.00350592 0.00295512 0.00275020 0.00265018 #NUM! #NUM! 0.00000000 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! 12 10 8 6 4 2 0 0 2 4 6 8 10 12 Crew Off Moment From Zero #NUM! Point #NUM! 0 Add FuelMoment Weight From Zero #NUM! #NUM! Point #NUM! #NUM! 0 0 Add Crew Moment Weight From Zero #NUM! #NUM! Point #NUM! #NUM! 0 0 Add Passenger Moment Weight From Zero #NUM! #NUM! Point #NUM! #NUM! 0 0 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 0 0 0 0 0 0 0 0 0 0 0 #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 0 0 0 0 0 0 0 0 0 0 #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! 0 798.17 214.15 0 40.4 84.66 283.58 456.01 198 #NUM! #NUM! 586.26 #NUM! 269.55 #NUM! 0 0 ­719.43 700 234 34 34 34 34 34 34 34 34 34 30 90 #NUM! 195 195 195 195 195 195 195 195 195 234 #NUM! #NUM! 0 #NUM! 2355.66 0 1737.2 3640.3 #NUM! 5016.16 8514 #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! #NUM! ­30935.49 #NUM! 4680 567.8 601.8 865.64 1031.39 531.42 1031.39 736.1 1152.6 442 600 3870 #NUM! 3256.5 3451.5 4964.7 5915.33 3047.85 5915.33 4221.75 4221.75 4221.75 #NUM! #NUM! #NUM! #NUM! 3499.51 #NUM! 3699.51 #NUM! 3699.51 #NUM! 3700 Wo W/S T/W=0.3 T/W=0.4 T/W=0.5 70 21813.00 21860 21890 90 21390.00 21430 21460 110 21100.00 21140 21170 Plots for T/W Contours 70 21813.00 90 21390.00 110 21100.00 74 94 114 78 98 118 21860 21430 21140 22000.00 21890 21460 21170 21800.00 21600.00 21400.00 21200.00 21000.00 20800.00 20600.00 70 75 80 85 90 Plots for W/S Contours 70 21813.00 74 21860 78 21890 90 21390.00 94 21430 98 21460 110 21100.00 114 21140 118 21170 95 100 105 1 plot for Top of Climb top of W/S [lb/ft2] climb 70 23017.63 90.0 23149.52 110.0 23253.39 plot for 2g manuever W/S [lb/ft2] 2g manuever 70.0 23017.63 90.0 23149.52 110.0 23253.39 plot for take off ground roll W/S [lb/ft2] take off ground roll 70.0 23017.63 90 23149.52 110 23253.39 plots for landing ground roll W/S [lb/ft2] Landing groud roll 70 23017.63 90 23149.52 110 23253.39 Column B Column C Column D Column B Column C Column D 80 85 90 95 100 105 110 115 120 ...
View Full Document

This document was uploaded on 10/24/2010.

Ask a homework question - tutors are online