RATE OF CHANGE OF CIRCULATION: KELVIN’S THEOREM

Consider the circulation around a fluid curve (which always passes through the same fluid particles) in an incompressible inviscid flow with conservative body

Подпись: DY Dt image42 Подпись: lcDI Подпись: d + Jc Dt Подпись: (2.13)

forces acting. The time rate of change of the circulation of this fluid curve C is given as

Подпись: Dq Dt Подпись: a Подпись: and Подпись: ~ d = dq Dt 4

Since C is a fluid curve, we have

and therefore

Подпись: DY Dt image43(2.14)

since the closed integral of an exact differential that is a function of the coordinates and time only is <J>C q • dq = <J>C d(q2/2) = 0. The acceleration a is obtained from the Euler equation (Eq. (1.62)) and is

—v(£)+r

Substitution into Eq. (2.14) yields the result that the circulation of a fluid curve remains constant:

Подпись: FIGURE 2.5 Circulation caused by an airfoil after it is suddenly set into motion.

since the integral of a perfect differential around a closed path is zero and the work done by a conservative force around a closed path is also zero. The result in Eq. (2.15) is a form of angular momentum conservation and is known as Kelvin’s theorem (after the British scientist who published his theorem in 1869), which states that: the time rate of change of circulation around a closed curve consisting of the same fluid elements is zero. For example, consider an airfoil as in Fig. 2.5, which prior to t = 0 was at rest and then at f>0 was suddenly set into a constant forward motion. As the airfoil moves through the

fluid a circulation rairfoii develops around it. In order to comply with Kelvin’s theorem a starting vortex Twake must exist such that the total circulation around a line that surrounds both the airfoil and the wake remains unchanged:

^ P ^airfoil "1" Pvake 1Л

d7“ Ї,————– “° (116)

This is possible only if the starting vortex circulation will be equal to the airfoil’s circulation, but its rotation will be in the opposite direction.