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In aerodynamics, the Crow instability is an inviscid line-vortex instability, named after its discoverer S. C. Crow. It is observed when the vortices caused by aircraft are being whirled from being otherwise straight contrails into spirals then donut-shaped rings.
See also
references
- Crow, S. C., Stability theory for a pair of trailing vortices, AIAA J., 8, 2172-2179 (1970).
- Saffman, P. G., Vortex Dynamics, Cambridge Uni. Press, New York (1992).
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This article is licensed under the GNU Free Documentation License.
Last updated on Friday April 04, 2008 at 08:06:32 PDT (GMT -0700)
View this article at Wikipedia.org - Edit this article at Wikipedia.org - Donate to the Wikimedia Foundation
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