title: Effect of outer wing separation on lift and thrust generation in a flapping wing system.
abstract: We explore the implementation of wing feather separation and lead-lagging motion to a flapping wing. A biomimetic flapping wing system with separated outer wings is designed and demonstrated. The artificial wing feather separation is implemented in the biomimetic wing by dividing the wing into inner and outer wings. The features of flapping, lead-lagging, and outer wing separation of the flapping wing system are captured by a high-speed camera for evaluation. The performance of the flapping wing system with separated outer wings is compared to that of a flapping wing system with closed outer wings in terms of forward force and downward force production. For a low flapping frequency ranging from 2.47 to 3.90 Hz, the proposed biomimetic flapping wing system shows a higher thrust and lift generation capability as demonstrated by a series of experiments. For 1.6 V application (lower frequency operation), the flapping wing system with separated wings could generate about 56% higher forward force and about 61% less downward force compared to that with closed wings, which is enough to demonstrate larger thrust and lift production capability of the separated outer wings. The experiments show that the outer parts of the separated wings are able to deform, resulting in a smaller amount of drag production during the upstroke, while still producing relatively greater lift and thrust during the downstroke.
authors.affiliation: Department of Advanced Technology Fusion, Konkuk University, Seoul, Korea.
authors.forename: Nanang
authors.initials: N
authors.lastname: Mahardika
authors.forename: Nguyen Quoc
authors.initials: NQ
authors.lastname: Viet
authors.forename: Hoon Cheol
authors.initials: HC
authors.lastname: Park
mesh_terms: D000401:Aircraft; D000818:Animals; D040761:Biomimetic Materials; D032701:Biomimetics / Q000295:instrumentation* / Q000379:methods*; D001717:Birds / Q000502:physiology*; D003198:Computer Simulation; D017076:Computer-Aided Design; D004867:Equipment Design; D019544:Equipment Failure Analysis; D005426:Flight, Animal / Q000502:physiology*; D008904:Miniaturization; D008954:Models, Biological; D013314:Stress, Mechanical; D014921:Wings, Animal / Q000502:physiology*