u = − eπφ/m = − beπ2/c,

ch Ω = cos nθ = √ 1, sh Ω = i sin nθ = i √ eπ2/c,
eπ2/c + 1 eπ2/c + 1

(2)

e½π2/c = tan nθ, ½π ds= 2n.
c sin 2nθ

(3)

For a jet impinging normally on an infinite plane, as in fig. 6, n = 1,

e½π2/c = tan θ, ch (½πs/c) sin 2θ = 1,

(4)

sh ½πx/c = cot θ, sh ½πy/c = tan θ,

sh ½πx/c sh ½πy/c = 1, e½π(x + y)/c = e1/2 πx/c + e1/2 πy/c + 1.