(84) φtθ = C[T(uφ) - T(uθ)],
(85) φxθ = C cos η [S(uφ) - S(uθ)],
| (86) | φ | ( | y | ) | θ | = tan φ - C sec η | [ | I(uφ) - | ΔA | ] | ; | |
| x | ΔS |
Δ now denoting any finite tabular difference of the function between the initial and final (pseudo-) velocity.
Also the velocity vθ at the end of the arc is given by
(87) vθ = uθ sec θ cos η.
Treating this final velocity vθ and angle θ as the initial velocity vφ and angle φ of the next arc, the calculation proceeds as before (fig. 2).
In the long range high angle fire the shot ascends to such a height that the correction for the tenuity of the air becomes important, and the curvature φ - θ of an arc should be so chosen that φyθ the height ascended, should be limited to about 1000 ft., equivalent to a fall of 1 inch in the barometer or 3% diminution in the tenuity factor τ.
A convenient rule has been given by Captain James M. Ingalls, U.S.A., for approximating to a high angle trajectory in a single arc, which assumes that the mean density of the air may be taken as the density at two-thirds of the estimated height of the vertex; the rule is founded on the fact that in an unresisted parabolic trajectory the average height of the shot is two-thirds the height of the vertex, as illustrated in a jet of water, or in a stream of bullets from a Maxim gun.