The researchers in Aerodynamics know that there is not a unitary method
of investigation in this field. The first mathematical model of the air-
plane wing, the model meaning the integral equation governing the phe-
nomenon, was proposed by L. Prandtl in 1918. The integral equation
deduced by Prandtl, on the basis of some assumptions which will be
specified in the sequeL furnishes the circulation C(y) (see Chapter 6).
U sing the circulation, one calculates the lift and moment coefficients,
which are very important in Aerodynamics. The first hypothesis made by
Prandtl consists in replacing the wing by a distribution of vortices on
the plan-form D of the wing (i. e. the projection of the wing on the
plane determined by the direction of the uniform stream at infinity and
t he direction of the span of the wing). Since such a distribution leads
to a potential flow in the exterior of D and the experiences show that
downstream the flow has not this character, Prandtl introduces as a sup-
plementary hypothesis another vortices distribution on the trace of the
domain D in the uniform stream. The first kind of vortices are called
tied vortices and the second kind of vortices are called free vortices.