Canard tip vortex splitting in a canard-wing configuration - Experimental observations
Author:
Affiliation:
1. University of Pisa, Pisa 56126, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46804
Reference9 articles.
1. Pressure measurements on a forward-swept wing-canard configuration
2. Analysis of the Interaction Between Lifting Surfaces by Means of a Non-Linear Panel Method
3. Vortex-wing interaction of a close-coupled canard configuration
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1. Wandering of a Wing-Tip Vortex: Rapid Scanning and Correction of Fixed-Point Measurements;Journal of Aircraft;2017-09
2. Wing Tip Vortex in the Near Field: An Experimental Study;Journal of Aircraft;2005-09
3. Expanding the role of the wind-driven manipulator;1997 World Aviation Congress;1997-08-22
4. Flow visualization of low speed perpendicular vortex-airfoil interaction;14th Applied Aerodynamics Conference;1996-06-17
5. High aspect ratio wings - Tip vortex structure and its numerical implications;Fluid Dynamics Conference;1996-06-17
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