Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism

Flapping flight shows promise for micro air vehicle design because flapping wings provide superior aerodynamic performance than that of fixed wings and rotors at low Reynolds numbers. In these flight regimes, unsteady effects become increasingly important. This thesis explores some of the unsteady e...

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Bibliographic Details
Main Author: Naegle, Nathaniel Stephen
Format: Others
Published: BYU ScholarsArchive 2012
Subjects:
PIV
MAV
Online Access:https://scholarsarchive.byu.edu/etd/3278
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd