j = 0;
为w = W_takeoff: -50: W_landing
j = + 1;
V (j, 1 =√(2 * w /ρ/ S / cl_max);
D (j, 1) = 0.5 *ρ* V (j) * (j) * * cd_max;
T (j, 1) = D (j);%的稳定水平飞行条件
F (j, 1) = ct * T (j);%的燃料消耗
重量(j, 1) = w;
t (j, 1) = abs((-10000)重量(j)) / F (j);
R (j, 1) = V (j) * t (j);
结束
W =重量;
T =表(V, D, F, W, T)
T =
81年×表5
VDFWt
________________________________
55.133 817.37 0.81737 10000 0
61.479 54.995 813.28 0.81328 9950
123.58 54.857 809.19 0.80919 9900
186.31 54.718 805.11 0.80511 9850
249.68 54.579 801.02 0.80102 9800
:::::
7498.5 43.412 506.77 0.50677 6200
7658.9 43.236 502.68 0.50268 6150
43.06 498.59 0.49859 6100 7822
7987.8 42.883 494.51 0.49451 6050
8156.3 42.706 490.42 0.49042 6000