Stability theory for a pair of trailing vortices

AIAA Journal

Volumn 8, Issue 12, 1970, Pages 2172-2179

  Crow, S C ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS, STABILITY; AIAJA; AR; FLOW OF FLUIDS; WAKES;

EID: 0014892585     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.6083     Document Type: Article

References (11)

1. Spreiter, J. R. and Sacks, A. H., “The Rolling Up of the Trailing Vortex Sheet and Its Effect on the Downwash behind Wings,”Journal of the Aeronautical Sciences, Vol. 18, No. 1, Jan. 1951, pp. 21-32.
2. Smith, T. B. and Beesmer, K. M., “Contrail Studies of Jet Aircraft,” ASTIA AD 217 188, April 1959, Meteorology Research Inc., Pasadena, Calif.
3. Scorer, R. S., Natural Aerodynamics, Pergamon Press, New York, 1958, pp. 73-75.
4. Batchelor, G. K., An Introduction to Fluid Dynamics, Cambridge University Press, Cambridge, England, 1967, p. 509.
5. Rosenhead, L., “The Spread of Yorticity in the Wake behind a Cylinder,”Proceedings of the Royal Society, Ser. A, Vol. 127,1930, pp. 590-612.
6. Hama, F. R., “Progressive Deformation of a Curved Vortex Filament by its Own Induction,”The Physics of Fluids, Vol. 5, No. 10, Oct. 1962, pp. 1156-1162.
7. Thomson, Sir W., “Vibrations of a Columnar Vortex,”Mathematical and Physical Payers, Vol. 4, Cambridge University Press, Cambridge, England, 1910, pp. 152-165.
8. Jahnke, E. and Emde, F., Tables of Functions,4th ed., Dover, New York, 1945, pp. 3-9.
9. Watson, G. N., Theory of Bessel Functions,2nd ed., Cambridge University Press, Cambridge, England, 1952, pp. 698-713.
10. Lamb, Sir H., Hydrodynamics,6th ed., Cambridge University Press, Cambridge, England, 1932, p. 241.
11. Tung, C. and Ting, L., “Motion and Decay of a Vortex Ring,” The Physics of Fluids, Vol. 10, No. 5, May 1967, pp. 901-910.