The initial (and quite brief) presence of a starting vortex as an airfoil begins to move was predicted by early aerodynamicists, and eventually photographed.

Whenever the speed or angle of attack of an airfoil changes there is a corresponding amount of vorticity deposited in the wake behind the airfoil, joining the two trailing vortices. This vorticity is a continuum of mini-starting-vortexes. The wake behind an aircraft is a continuous sheet of weak vorticity, between the two trailing vortices, and this accounts for the changes in strength of the trailing vortices as the airspeed of the aircraft and angle of attack on the wing change during flight. (The strength of a vortex cannot change within the fluid except by the dissipative action of viscosity. Vortices either form continuous loops of constant strength, or they terminate at the boundary of the fluid - usually a solid surface such as the ground.)

The starting vortex is significant to an understanding of the Kutta condition and its role in the circulation around any airfoil generating lift.

The starting vortex has certain similarities with the 'starting plume' which forms at the leading edge of a slug of fluid, when one fluid is injected into another at rest - see plume (hydrodynamics)

References

• Clancy, L.J. (1975), Aerodynamics, Section 4.8, Pitman Publishing Limited, London ISBN 0 273 01120 0
• Millikan, Clark B., Aerodynamics of the Airplane, Section 1-6, eighth printing, John Wiley and Sons, Inc., (1941) New York.
• Massey, B.S., Mechanics of Fluids, Section 9.10, 2nd Edition. Van Nostrand Reinhold Co., London (1970) Library of Congress Catalog Card No. 67-25005

See also

• Helmholtz's theorems
• Kutta condition
• Kutta–Joukowski theorem