Morphing wing for an aircraft
作者： Amin Moosavian , Allan Daniel Finistauri , Fengfeng Xi
DOI:
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摘要: A morphing wing for an aircraft includes a top surface, bottom leading edge, trailing tip, and root. plurality of structural ribs (76,78) is disposed between the root tip so that they extend surface intersect with lateral axis thereof. At least one active member (88,90,92,94) connects two adjacent along or at first angle to axis. The actively adjustable. passive (80,82,84,86) second passively Adjustment moves respect another, thereby from configuration configuration.
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