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- W2362393565 abstract "The most critical geometric parameters of winglets in drag reduction efficiency were summarized.Then the numerical simulation method was utilized to reveal the optimal range of these parameters,which is the theoretical basis of morphing winglet design.The advantages and disadvantages of morphing winglets in aerodynamic performance,aerodynamic load distribution and wingtip vortices were discussed compared with traditional winglets. The results show that morphing winglets can increase the drag reduction efficiency by 2.2% compared with traditional winglets and weaken the wingtip vortices by 15%in the takeoffphase of flight.It is beneficial to enhance the fuel efficiency of aircraft and the airport spatial security.However,morphing winglets increase the bending moment at the wing root.For this reason,aircraft designers have to strik a balance between the aerodynamic benefits and the structural disadvantages in morphing winglet designs." @default.
- W2362393565 created "2016-06-24" @default.
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- W2362393565 date "2014-01-01" @default.
- W2362393565 modified "2023-09-23" @default.
- W2362393565 title "Numerical simulation on morphing winglets for its drag reduction mechanisms" @default.
- W2362393565 hasPublicationYear "2014" @default.
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