Rapid Scanning, Three-Dimensional Hot-Wire AnemometerSurveys of Wing-Tip Vortices
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
2. Nielsen Engineering and Research, Inc., Mountain View, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60301
Reference16 articles.
1. Wind-Tunnel Studies of Wing Wake Turbulence
2. 3Mason, W. H. and Marchman, J. F. "Farfield Structure of an Aircraft Trailing Vortex, Including Effects of Mass Injection," CR-62078,1972, NASA.
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