Drag reduction analysis of wing airfoil E562 with forward wingtip fence at cant angle variations of 75° and 90°

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P. Setyo Hariyadi S.,Sutardi ,Widodo Wawan Aries

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Reference10 articles.

1. Hemke, P.E., Drag of Wings with End Plates, NASA-Report, No 267, 1928.

2. Dinesh M.; Kenny Mark V.; Dharni Vasudhevan Venkatesan; Santhosh Kumar B.; Sree Radesh R.; V. R. Sanal Kumar, Diagnostic Investigation of Aircraft Performance at Different Winglet Cant Angles, World Academy of Science, Engineering and Technology International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering Vol:8, No:12, 2014

3. Numerical study of aerodynamic analysis on wing airfoil NACA 43018 with the addition of forward and rearward wingtip fence

4. Mulvany, Nicholas J., Li Chen, Jiyuan Y. Tu and Anderson, Brendon, Steady State Evaluation of Two Equation RANS Turbulence Models for High Reynolds Number Hydrodynamic Flow Simulations, Final Report, Defence Science and Technology Organisation, Departement of Defence, Australian Government, 2004

5. Anderson. J. D., Jr., Computational Fluid Dynamics, Mc-Graw Hill. New York, 1995

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