Wing Taper Considerations Tapering a wing planform gives a number of signiﬁcant aerodynamic and structural advantages, but it can also cause problems if overdone. Consider three AR = 10 wings of the same span and area, but diﬀerent taper ratios λ = ctip croot . When operated at some overall lift - Aerodynamic - Document - PDFSEARCH.IO

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Date: 2013-09-29 08:11:09 Fluid dynamics Washout Stall Wing twist Chord Lift-induced drag Stall strips Aerospace engineering Aerodynamics Aviation		Wing Taper Considerations Tapering a wing planform gives a number of signiﬁcant aerodynamic and structural advantages, but it can also cause problems if overdone. Consider three AR = 10 wings of the same span and area, but diﬀerent taper ratios λ = ctip /croot . When operated at some overall lift Add to Reading List Source URL: ocw.mit.edu Download Document from Source Website File Size: 42,37 KB Share Document on Facebook

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