Structural Design and Analysis of a Kinematic Mechanism for a Morphing Hyper-Elliptic Cambered Span (HECS) Wing
The HECS wing was developed by NASA Langley Research Center and has a nonplanar, hyper-elliptically swept leading and trailing edge as well as spanwise camber. For this wing, the leading and trailing edges are swept back according to a hyper-elliptical equation. The span of the wing is also defined...
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| Format: | Others |
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Virginia Tech
2011
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| Online Access: | http://hdl.handle.net/10919/9668 http://scholar.lib.vt.edu/theses/available/etd-01062004-145409 |