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Stall strips
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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
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Source URL: ocw.mit.edu
Language: English
- Date: 2013-09-29 08:11:09
Fluid dynamics
Washout
Stall
Wing twist
Chord
Lift-induced drag
Stall strips
Aerospace engineering
Aerodynamics
Aviation
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