Further Development of the Kinematic and Aerodynamic Modeling and Analysis of Flapping Wing Ornithopter from Basic Principles
The basis of this work was to understand the generation of lift and thrust of a flapping bi-wing ornithopter, which is influenced by its geometrical, dynamic, kinematic and aerodynamic features by following a generic approach in order to identify and mimic the mechanisms. As further development of e...
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Veröffentlicht in: | Applied Mechanics and Materials 2014-10, Vol.629 (AEROTECH V: Progressive Aerospace Research), p.9-17 |
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Format: | Artikel |
Sprache: | eng |
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