<<<<<<<<<<<< Input Data >>>>>>>>>>>>>> dc9 jan 26 example Mar 97 run Atmospheric density = 0.002377 (sl/ft^2) Aircraft Weight = 95000.000000 (lbs) Wing area = 1000.000000 (ft^2) Maximum lift coefficient = 2.000000 Ground lift coefficient = 0.300000 Air lift coefficient = 1.650000 Ground drag coefficient = 0.080000 Air drag coefficient = 0.121000 Rolling friction coeff. = 0.025000 Braking friction coeff. = 0.300000 Angle of thrust = 0.000000 (rad) Stall margin (k) = 1.100000 Descision time = 3.000000 (sec) Obstacle height = 35.000000 (ft) OEI power remaining = 0.500000 Thrust = 31450.000000 + -17.263404 * V + 0.025019 * V^2 Normal Takeoff >>>>>>>>>>>>>> Time (s) x-dist (ft) x-Vel (ft/s) y-dist (ft) y-Vel (ft/s) 0.000 0.000 0.000 0.000 0.000 1.000 4.914 9.818 0.000 0.000 2.507 30.796 24.499 0.000 0.000 4.251 88.171 41.290 0.000 0.000 6.015 175.840 58.058 0.000 0.000 7.679 285.433 73.650 0.000 0.000 9.032 393.639 86.169 0.000 0.000 10.276 507.915 97.533 0.000 0.000 11.411 624.341 107.772 0.000 0.000 12.443 740.367 116.989 0.000 0.000 13.385 854.499 125.311 0.000 0.000 14.248 965.973 132.864 0.000 0.000 15.044 1074.493 139.762 0.000 0.000 15.783 1180.041 146.104 0.000 0.000 16.472 1282.758 151.972 0.000 0.000 17.119 1382.861 157.438 0.000 0.000 17.730 1480.600 162.558 0.000 0.000 18.310 1576.227 167.380 0.000 0.000 18.862 1669.986 171.944 0.000 0.000 19.391 1762.097 176.282 0.000 0.000 19.900 1852.764 180.423 0.000 0.000 20.390 1942.163 184.389 0.000 0.000 20.864 2030.452 188.198 0.000 0.000 21.323 2117.769 191.869 0.000 0.000 21.770 2204.232 195.413 0.000 0.000 22.204 2289.945 198.844 0.000 0.000 22.629 2374.997 202.170 0.000 0.000 23.043 2459.465 205.401 0.000 0.000 23.449 2543.417 208.545 0.000 0.000 23.846 2626.910 211.607 0.000 0.000 24.236 2709.994 214.594 0.000 0.000 24.619 2792.713 217.510 0.000 0.000 24.936 2862.147 219.912 0.000 0.000 27.936 3555.391 242.080 0.000 0.000 28.000 3570.887 242.517 0.014 0.436 28.084 3591.316 243.084 0.075 1.025 28.189 3616.811 243.777 0.222 1.781 28.314 3647.263 244.583 0.502 2.715 28.457 3682.379 245.482 0.971 3.832 28.617 3721.746 246.449 1.687 5.135 28.792 3764.890 247.460 2.713 6.620 28.979 3811.319 248.489 4.107 8.284 29.177 3860.555 249.511 5.925 10.118 29.383 3912.155 250.505 8.218 12.115 29.596 3965.718 251.451 11.032 14.264 29.815 4020.894 252.331 14.405 16.552 30.039 4077.380 253.132 18.373 18.969 30.266 4134.917 253.842 22.965 21.503 30.496 4193.289 254.450 28.205 24.140 30.727 4252.316 254.948 34.114 26.869 30.961 4260.314 254.999 35.000 27.246 n<<<<<<<<<<<<<< Normal Take-off Summary >>>>>>>>>>>>>>> Rotation Velocity = 219.912 (ft/s) Lift-off velocity = 242.080 (ft/s) Velocity over obstacle = 256.451 (ft/s) Rotation distance = 2862.147 (ft) Lift-off distance = 3555.391 (ft) Distance to obstacle = 4260.314 (ft) Rotation time = 24.936 (s) Lift-off time = 27.936 (s) Time to obstacle = 30.759 (s) n<<<<<<<<<<<<<<<<<<<<<<< OEI Take-Off Summary >>>>>>>>>>>>>>>>>>>> Critical Velocity = 203.886 (ft/s) Decision Velocity = 212.381 (ft/s) Velocity over obstacle = 233.529 (ft/s) Critical Distance = 2419.709 (ft) Decision Distance = 3044.195 (ft) Balanced Field Length = 5398.148 (ft) Critical Time = 22.849 (sec) Decision Time = 25.849 (sec) OEI Takeoff Time = 36.300 (sec)