Ontogeny of aerial righting and wing flapping in juvenile birds [PDF]
Mechanisms of aerial righting in juvenile Chukar Partridge (Alectoris chukar) were studied from hatching through 14 days post hatching (dph). Asymmetric movements of the wings were used from 1 to 8 dph to effect progressively more successful righting ...
Cam, Sharlene +4 more
core +3 more sources
Research and Test of X-wing Flapping-wing Mechanism Based on the Crank Slider Mechanism
A X-wing flapping-wing mechanism with wings flapping symmetrically is designed. The crank slider mechanism is adopted to convert the circular motion of the crank into the linear reciprocating motion of the straight shaft, and the straight shaft drives ...
Huang Xiansheng, Cai Yu, Li Qi, Liu Bin
doaj
Experimental investigation of some aspects of insect-like flapping flight aerodynamics for application to micro air vehicles [PDF]
Insect-like flapping flight offers a power-efficient and highly manoeuvrable basis for micro air vehicles for indoor applications. Some aspects of the aerodynamics associated with the sweeping phase of insect wing kinematics are examined by making ...
Ansari, S. A. +5 more
core +1 more source
Comparison of Power Requirements: Flapping vs. Fixed Wing Vehicles
The power required by flapping and fixed wing vehicles in level flight is determined and compared. Based on a new modelling approach, the effects of flapping on the induced drag in flapping wing vehicles are mathematically described.
Gottfried Sachs
doaj +1 more source
A linear systems analysis of the yaw dynamics of a dynamically scaled insect model [PDF]
Recent studies suggest that fruit flies use subtle changes to their wing motion to actively generate forces during aerial maneuvers. In addition, it has been estimated that the passive rotational damping caused by the flapping wings of an insect is ...
Dickinson, Michael H. +3 more
core +1 more source
Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft
Aiming at the problems of single flapping wing movement mode and low flight flexibility and stability of flapping-wing aircraft, a single-drive multi-mode flapping-wing aircraft based on the space linkage mechanism is designed. The kinematic model of the
Jiang Houqing, Hou Yu, Guo Yongxing
doaj
Flight performance calculation is an important part of the micro flapping wing air vehicle design. It is used to verify whether the air vehicle design meets the performance requirements so as to make targeted improvements to the design.
Jianlin Xuan, Z. Yang, P. Nian, D. Ma
doaj +1 more source
Design of Variable Amplitude Flapping Wing Aircraft and Realization of Multiple Flight Modes
Aiming at the problems of the single flight mode and inflexible flight attitudeļ¼a variable amplitude flapping wing aircraft is designed. By adjusting the flapping amplitudeļ¼ the flapping wing motion attitude and flight mode can be switched.
Yueyang Hou +4 more
doaj
Effects of deformation and vibration characteristics of wings on flapping flight
The dragonfly wing is passively deformed under flapping and has the strength to withstand high flapping frequency simultaneously. These characteristics of deformation and vibration of the wing are important for flapping flight.
Hisayoshi NAKA, Hiromu HASHIMOTO
doaj +1 more source
Towards Bio-Inspiration, Development, and Manufacturing of a Flapping-Wing Micro Air Vehicle
Throughout the last decade, there has been an increased demand for intricate flapping-wing drones with different capabilities than larger drones. The design of flapping-wing drones is focused on endurance and stability, as these are two of the main ...
P. Lane +5 more
doaj +1 more source

