Three-dimensional numerical simulation of a bird model in unsteady flight

被引:6
作者
Zhu Lin-Lin [1 ]
Guan Hui [2 ]
Wu Chui-Jie [1 ]
机构
[1] Dalian Univ Technol, Sch Aeronaut & Astronaut, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Liaoning, Peoples R China
[2] PLA Univ Sci & Technol, Coll Meteorol & Oceanog, Nanjing 211101, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
Self-propelled flying; Flapping wings; Numerical simulation; Three-dimensional; SPACE-TIME PROCEDURE; MOVING BOUNDARIES; REVOLVING WINGS; HOVERING FLIGHT; FLAPPING WINGS; AERODYNAMICS; FLOWS; COMPUTATIONS; FORCE; LIFT;
D O I
10.1007/s00466-015-1233-3
中图分类号
O1 [数学];
学科分类号
0701 ; 070101 ;
摘要
In this paper, a type of numerical simulation of a three-dimensional (3D) bionic bird with flapping wings in a viscous flow is studied. The model is a self-propelled flying bird capable of free rotation and translation whose flying motion follows the laws of conservation of momentum and angular momentum. The bird is propelled and lifted through flapping and rotating wings and most of thrust force and lift force are exerted on both wings. Both the vortex structures and the flight characteristics are also presented. The relationship between both wings' movement and the vortex structures as well as that between both wings' movement and flight characteristics are also analyzed in this paper. The study uses a 3D computational fluid dynamics package that includes the combined immersed boundary method, volume of fluid method, adaptive multigrid finite volume method, and control strategy for swimming and flying.
引用
收藏
页码:1 / 11
页数:11
相关论文
共 44 条
[1]  
[Anonymous], 1988, STUDYING TURBULENCE
[2]   Insectlike Flapping Wings in the Hover Part 1: Effect of Wing Kinematics [J].
Ansari, Salman A. ;
Knowles, Kevin ;
Zbikowski, Rafal .
JOURNAL OF AIRCRAFT, 2008, 45 (06) :1945-1954
[3]   Aerodynamic and FSI Analysis of Wind Turbines with the ALE-VMS and ST-VMS Methods [J].
Bazilevs, Yuri ;
Takizawa, Kenji ;
Tezduyar, Tayfun E. ;
Hsu, Ming-Chen ;
Kostov, Nikolay ;
McIntyre, Spenser .
ARCHIVES OF COMPUTATIONAL METHODS IN ENGINEERING, 2014, 21 (04) :359-398
[4]   EULER CALCULATIONS FOR MULTIELEMENT AIRFOILS USING CARTESIAN GRIDS [J].
CLARKE, DK ;
SALAS, MD ;
HASSAN, HA .
AIAA JOURNAL, 1986, 24 (03) :353-358
[5]   Wing rotation and the aerodynamic basis of insect flight [J].
Dickinson, MH ;
Lehmann, FO ;
Sane, SP .
SCIENCE, 1999, 284 (5422) :1954-1960
[6]   Wake topology and hydrodynamic performance of low-aspect-ratio flapping foils [J].
Dong, H. ;
Mittal, R. ;
Najjar, F. M. .
JOURNAL OF FLUID MECHANICS, 2006, 566 :309-343
[7]   Leading-edge vortices in insect flight [J].
Ellington, CP ;
vandenBerg, C ;
Willmott, AP ;
Thomas, ALR .
NATURE, 1996, 384 (6610) :626-630
[8]   LAGRANGIAN-EULERIAN FINITE-ELEMENT FORMULATION FOR INCOMPRESSIBLE VISCOUS FLOWS [J].
HUGHES, TJR ;
LIU, WK ;
ZIMMERMANN, TK .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1981, 29 (03) :329-349
[9]  
Iaccarino G., 2003, Applied Mechanics Review, V56, P331, DOI 10.1115/1.1563627
[10]  
Iaccarino G, 2003, 20030770 AIAA