Computational fluid-structure interaction framework for passive feathering and cambering in flapping insect wings

被引:3
|
作者
Ishihara, Daisuke [1 ]
Onishi, Minato [2 ]
机构
[1] Kyushu Inst Technol, Dept Intelligent & Control Syst, 680-4 Kawazu, Iizuka, Fukuoka 8208502, Japan
[2] Kyushu Inst Technol, Dept Comp Sci & Syst Engn, Iizuka, Fukuoka, Japan
基金
日本学术振兴会;
关键词
cambering; feathering; fluid-structure interaction; insect flapping flight; passive mechanism; pixel model; INCOMPRESSIBLE VISCOUS-FLUID; FINITE-ELEMENT FORMULATION; IMMERSED BOUNDARY METHOD; MONOLITHIC APPROACH; LIFT GENERATION; DESERT LOCUST; LINE-SEARCH; FLIGHT; AERODYNAMICS; KINEMATICS;
D O I
10.1002/fld.5251
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In flapping insect wings, veins support flexible wing membranes such that the wings form feathering and cambering motions passively from large elastic deformations. These motions are essentially important in unsteady aerodynamics of insect flapping flight. Hence, the underlying mechanism of this phenomenon is an important issue in studies on insect flight. Systematic parametric studies on strong coupling between a model wing describing these elastic deformations and the surrounding fluid, which is a direct formulation of this phenomenon, will be effective for solving this issue. The purpose of this study is to develop a robust numerical framework for these systematic parametric studies. The proposed framework consists of two novel numerical methods: (1) A fully parallelized solution method using both algebraic splitting and semi-implicit scheme for monolithic fluid-structure interaction (FSI) equation systems, which is numerically stable for a wide range of properties such as solid-to-fluid mass ratios and large body motions, and large elastic deformations. (2) A structural mechanics model for insect flapping wings using pixel modeling (pixel model wing), which is combined with explicit node-positioning to reduce computational costs significantly in controlling fluid meshes. The validity of the proposed framework is demonstrated for some benchmark problems and a dynamically scaled model incorporating actual insect data. Finally, from a parametric study for the pixel model wing flapped in fluid with a wide range of solid-to-fluid mass ratios, we find a FSI mechanism of feathering and cambering motions in flapping insect wings. We developed a novel computational framework that consists of a fully parallelized solution method using algebraic splitting and semi-implicit scheme for monolithic FSI equation systems, the parallel CG method, and a pixel model wing combined with explicit node-positioning.Using the proposed framework, we found that feathering and cambering motions in flapping insect wings will be given based on the equilibrium between wing's elastic and aerodynamic forces, and these motions are enhanced by the wing's inertial force.image
引用
收藏
页码:435 / 481
页数:47
相关论文
共 50 条
  • [41] A complementary study of analytical and computational fluid-structure interaction
    Michael Andre
    Kai-Uwe Bletzinger
    Roland Wüchner
    Computational Mechanics, 2015, 55 : 345 - 357
  • [42] A complementary study of analytical and computational fluid-structure interaction
    Andre, Michael
    Bletzinger, Kai-Uwe
    Wuechner, Roland
    COMPUTATIONAL MECHANICS, 2015, 55 (02) : 345 - 357
  • [43] Computational fluid-structure interaction model for parachute inflation
    Benney, RJ
    Stein, KR
    JOURNAL OF AIRCRAFT, 1996, 33 (04): : 730 - 736
  • [44] COMPUTATIONAL FLUID-STRUCTURE INTERACTION FOR BIOLOGICAL AND BIOMEDICAL FLOWS
    Tian, F. B.
    Dai, H.
    Luo, H.
    Doyle, J. F.
    Rousseau, B.
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING, 2013, VOL 1A: SYMPOSIA, 2014,
  • [45] A COMPUTATIONAL ANALYSIS OF FLUID-STRUCTURE INTERACTION IN METACHRONAL PROPULSION
    Lou, Zhipeng
    Lei, Menglong
    Byron, Margaret L.
    Li, Chengyu
    PROCEEDINGS OF ASME 2024 FLUIDS ENGINEERING DIVISION SUMMER MEETING, VOL 2, FEDSM 2024, 2024,
  • [46] Vanguard developments in computational methods for fluid-structure interaction
    van Brummelen, E. Harald
    Farhat, Charbel
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2021, 122 (19) : 5173 - 5175
  • [47] COMPUTATIONAL FLUID-STRUCTURE INTERACTION OF DGB PARACHUTES IN COMPRESSIBLE FLUID FLOW
    Pantano-Rubino, Carlos
    Karagiozis, Kostas
    Kamakoti, Ramji
    Cirak, Fehmi
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER MEETING - 2010 - VOL 3, PTS A AND B, 2010, : 309 - 315
  • [48] Experimental investigation of fluid-structure interaction in a bird-like flapping wing
    Deshpande, Parag
    Modani, Amrut
    JOURNAL OF FLUIDS AND STRUCTURES, 2019, 91
  • [49] Line search partitioned approach for fluid-structure interaction analysis of flapping wing
    University of Tokyo, Bunkyo, Tokyo, Japan
    CMES Comput. Model. Eng. Sci., 2008, 1 (51-60):
  • [50] Special issue on computational fluid mechanics and fluid-structure interaction Preface
    Bazilevs, Yuri
    Takizawa, Kenji
    Tezduyar, Tayfun E.
    COMPUTATIONAL MECHANICS, 2011, 48 (03) : 245 - 245