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- W2384682489 abstract "The wind tunnel force measurements are conducted to investigate the influence of wing planforms(sweep angles) on aerodynamic characteristics of MAV with spanwise length to root chord length ratio of 1.0.The experimental results indicate that the wings of Λ=0-35 deg increase the maximum lift coefficient and the stalling angle,and delay stall.The wings of Λ=56-64 deg have better lift curve,but decrease the stalling angle.Otherwise,in comparison with the wing with leading edge beveled windward,the wing with leading edge beveled leeward can greatly improve the lift-to-drag ratio and the maximum lift coefficient after the stall of the wings." @default.
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- W2384682489 date "2007-01-01" @default.
- W2384682489 modified "2023-09-27" @default.
- W2384682489 title "The effects of wing planforms on aerodynamics of MAV" @default.
- W2384682489 hasPublicationYear "2007" @default.
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