期刊
ACTA MECHANICA SINICA
卷 26, 期 6, 页码 863-879出版社
SPRINGER HEIDELBERG
DOI: 10.1007/s10409-010-0389-5
关键词
Micro air vehicle; Bio-flight; Computational mechanics; Integrative biomechanics
资金
- PRESTO-JST program
- JSPS, Japan [18656056, 18100002]
- CKSP scholarship
- MEXT
- Air Force Office of Scientific Research's Multidisciplinary University Research Initiative (MURI)
- Michigan/AFRL (Air Force Research Laboratory)/Boeing Collaborative Center in Aeronautical Sciences
- Grants-in-Aid for Scientific Research [18100002, 18656056] Funding Source: KAKEN
Aiming at developing an effective tool to unveil key mechanisms in bio-flight as well as to provide guidelines for bio-inspired micro air vehicles (MAVs) design, we propose a comprehensive computational framework, which integrates aerodynamics, flight dynamics, vehicle stability and maneuverability. This framework consists of (1) a Navier-Stokes unsteady aerodynamic model; (2) a linear finite element model for structural dynamics; (3) a fluid-structure interaction (FSI) model for coupled flexible wing aerodynamics aeroelasticity; (4) a free-flying rigid body dynamic (RBD) model utilizing the Newtonian-Euler equations of 6DoF motion; and (5) flight simulator accounting for realistic wing-body morphology, flapping-wing and body kinematics, and a coupling model accounting for the nonlinear 6DoF flight dynamics and stability of insect flapping flight. Results are presented based on hovering aerodynamics with rigid and flexible wings of hawkmoth and fruitfly. The present approach can support systematic analyses of bio- and bio-inspired flight.
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