Structure and Induced Drag of a Tip Vortex
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.2707
Reference21 articles.
1. 1Aviation Week and Space Technology, 23 June 2003, p. 15.
2. Turbulent line vortices
3. Axial flow in trailing line vortices
4. Viscous Modelling of Wing-Generated Trailing Vortices
5. Calculation of Aircraft Wake Velocity Profiles and Comparisonwith Experimental Measurements
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