Rapidly Growing Instability Mode in Trailing Multiple-Vortex Wakes
Author:
Affiliation:
1. University of California, Berkeley, Berkeley, California 94720-1740
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1375
Reference18 articles.
1. Stability theory for a pair of trailing vortices
2. Flight Test Studies of the Formation and Dissipation of Trailing Vortices
3. Barber, M. R., and Tymczyszyn, J. J. “Wake Vortex Attenuation Tests: A Status Report,” 1980Aircraft Safety and Operating Problems,NASA CP-2170, 1981, pp.387-408.
4. Lift-generated vortex wakes of subsonic transport aircraft
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