Przykładowe obliczenia dla kąta α=12° na wysokości 100m.
Prędkość lotu
Prędkość opadania
Kąt toru lotu
H=100 | H=1500 | H=4000 | ||||
---|---|---|---|---|---|---|
α | Cx | Cz | V | w | V | w |
12 | 0,20351 | 1,21393 | 37,6354 | 6,22259 | 40,3016 | 6,6634 |
11 | 0,18515 | 1,17487 | 38,2864 | 5,95998 | 40,9987 | 6,3822 |
10 | 0,16429 | 1,12656 | 39,1328 | 5,64731 | 41,905 | 6,04737 |
9 | 0,14865 | 1,07003 | 40,1727 | 5,52779 | 43,0185 | 5,91938 |
8 | 0,13214 | 1,0063 | 41,4461 | 5,39605 | 44,3822 | 5,77832 |
7 | 0,11775 | 0,93743 | 42,957 | 5,35373 | 46,0002 | 5,73299 |
6 | 0,10457 | 0,85725 | 44,9309 | 5,44031 | 48,1138 | 5,82571 |
5 | 0,10405 | 0,95182 | 42,6713 | 4,63721 | 45,6942 | 4,96572 |
4 | 0,08375 | 0,71335 | 49,268 | 5,74512 | 52,7582 | 6,15211 |
3 | 0,07515 | 0,61776 | 52,9297 | 6,39201 | 56,6793 | 6,84483 |
2 | 0,06737 | 0,51702 | 57,8255 | 7,47188 | 61,9219 | 8,0012 |
1 | 0,06076 | 0,41321 | 64,6094 | 9,3994 | 69,1864 | 10,0653 |
0 | 0,05538 | 0,31145 | 74,2386 | 12,9979 | 79,4978 | 13,9187 |