(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];
xΔS

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.