Experimental Study of the Effect of Span Loading on Aircraft Wakes
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58737
Reference20 articles.
1. Vortex Attenuation Obtained in the Langley Vortex Research Facility
2. Rapid Scanning, Three-Dimensional Hot-Wire AnemometerSurveys of Wing-Tip Vortices
3. Aircraft wake dissipation by sinusoidal instability and vortex breakdown
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