This research investigates the energy-efficient optimization of flapping wing micro aerial vehicle win geometry and corresponding optimal wing kinematics.
Structural Technology Evaluation and Analysis Program (STEAP). Delivery Order 0049: Computational Prototyping of Micro Air Vehicles
2013
54 pages
Report
Keine Angabe
Englisch
Aircraft , Physical & Theoretical Chemistry , Algebra, Analysis, Geometry, & Mathematical Logic , Quality Control & Reliability , Computations , Prototypes , Structural properties , Kinematics , Wings , Fsi(Flapping sciences integration) , Fwmuav(Flapping wing micro aerial vehicle) , M3ct(Model based computational tool) , Mpp(Multi physics prototyping) , Multidisciplinaries , Multifidelities
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