Optimization and analysis of winglet configuration for solar aircraft

Author:

ZHANG Liang,MA Dongli,YANG Muqing,WANG Shaoqi

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference40 articles.

1. Design of solar high altitude long endurance aircraft for multi payload & operations;Cestino;Aerosp Sci Technol,2006

2. Slooff JW. Computational methods for subsonic and transonic aerodynamic design. Proceeding of the first conference on inverse design concepts and optimization in engineering; 1983 Jan 20; Philadelphia, USA. Amsterdam: NLR; 1984

3. Effect of winglets induced tip vortex structure on the performance of subsonic wings;Narayan;Aerosp Sci Technol,2016

4. Whitcomb RT. A design approach and selected wind tunnel results at high subsonic speeds for wing-tip mounted winglets. Washington, D.C.: NASA Langley Research Center; 1976. Report No.: NASA-TN-D-8260.

5. Using wing tip devices to improve performance of saucer-shaped aircraft;Yu;Chin J Aeronaut,2006

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