A joint project of the Graduate School, Peabody College, and the Jean & Alexander Heard Library

Title page for ETD etd-01302013-191446

Type of Document Dissertation
Author Dai, Hu
Author's Email Address daihu000@gmail.com
URN etd-01302013-191446
Title Computational modeling of fluid–structure interaction in biological flying and swimming
Degree PhD
Department Mechanical Engineering
Advisory Committee
Advisor Name Title
Professor Haoxiang Luo Committee Chair
Professor Amrutur Anilkumar Committee Member
Professor Caglar Oskay Committee Member
Professor D. Greg Walker Committee Member
Professor Jon Edd Committee Member
  • immersed boundary method
  • biological flying/swimming
  • numerical modeling
  • insect flight
  • fluid-structure interaction
  • CFD
Date of Defense 2013-01-24
Availability unrestricted
Insects and fish in the animal world typically possess superior efficiency in locomotion, and they are capable of maneuvering in

complex environments full of unpredictable disturbances. Such locomotion modes have inspired biomimetic designs of unmanned aerial

and underwater vehicles. However, the fluid dynamics related to the flapping wings and fins is still a highly challenging problem as it

involves three-dimensional, unsteady, massively separated flows and it also has to do with significant deformation of the flexible wings and

fins. To date, the fundamental study on the role of the flexibility of the wings/fins in the animal propulsion is still very limited. In

this research, our objectives are: (1) to develop a versatile computational approach to model the fluid-structure interaction (FSI)

for various types of wings and fins, and (2) to study the effect of the structural deformation on the hydrodynamic performance of these

biological propulsors.

To achieve these objectives, we have developed an in-house FSI program. The code couples a viscous incompressible flow solver based

on the immersed-boundary method and a nonlinear finite-element solver for thin-walled structures. Using the Cartesian grid, the

sharp-interface immersed boundary method can treat the complex domain and moving boundaries in a straightforward manner. The solid-dynamics

solver has the capability of handling large displacements and large rotations of reinforced plate structures. Using this method, we

address the FSI of flapping wings/fins in three specific configurations: (1) a low-aspect-ratio elastic plate pitching in a

freestream, where a scaling law of the thrust production is obtained

based on the deformation mode of the plate; (2) an elastic rectangular

plate performing hovering motion, where the effect of dynamic pitching

due to the inertial and aerodynamic forces is investigated; and (3) a high-fidelity computational model of the cicada forewing, where the wing structure, the mechanical properties, and the wing kinematics of

the real insect are measured and the FSI model is validated against the high-speed imaging data. The results from these studies may

provide useful guidance for the engineering design of flexible propulsors.

  Filename       Size       Approximate Download Time (Hours:Minutes:Seconds) 
 28.8 Modem   56K Modem   ISDN (64 Kb)   ISDN (128 Kb)   Higher-speed Access 
  dissertation_Dai.pdf 4.81 Mb 00:22:17 00:11:27 00:10:01 00:05:00 00:00:25

Browse All Available ETDs by ( Author | Department )

If you have more questions or technical problems, please Contact LITS.