Aerodynamic effects of delta planform tip sails on wing performance
Author:
Affiliation:
1. University of the Witwatersrand, Johannesburg, South Africa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46626
Reference8 articles.
1. Winglet Toe-Out Angle Optimization for the Gates Learjet Longhorn Wing
2. Effect of Winglets on Performance and Handling Qualities of General Aviation Aircraft
3. Wing tip sails; progress to date and future developments
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