Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system

doi:10.1007/s11071-021-06486-0

CORC > 力学研究所 > 中国科学院力学研究所 > 高温气体动力学国家重点实验室

	Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system
	Zhu, Hong 4; Sun, Qinglin 4; Liu, Xuefeng 2,3; Liu, Jinglei 2,3; Sun, Hao 4; Wu WN(邬婉楠)1; Tan, Panlong 4; Chen, Zengqiang 4
刊名	NONLINEAR DYNAMICS
	2021-05-21
页码	22
关键词	Fluid-structure interaction Parafoil system Flexible deformation Trailing edge deflection Aerodynamic performance Dynamic model
ISSN号	0924-090X
DOI	10.1007/s11071-021-06486-0
通讯作者	Sun, Qinglin(sunql@nankai.edu.cn)
英文摘要	Prediction of aerodynamic force is a crucial issue for parafoil canopy as the strong nonlinear fluid-structure interaction (FSI) between the flexible canopy material and flow field. Flight tests and wind tunnel experiments are difficult to analyze the aerodynamics of parafoil because of the limitation and difficulty of data measurement in an unknown environment. The objective of this study was to computationally derive the aerodynamic characteristics of parafoil, as an alternative to expensive and unrepeatable test regimes. Different from previous works that assume canopy structure as a rigid body and serve for the design of parafoil, this study focused on the precise dynamic modeling of parafoil based on FSI simulations. To investigate the aerodynamic performance of the full-scale canopy with stabilizers for better control, the strong coupling FSI simulations were performed using the incompressible computational fluid dynamics techniques. The highlight of this paper is to explore the effects of canopy inflation and trailing edge deflections on aerodynamic performance. Then the aerodynamic coefficients are identified by a linear regression method using the obtained database of high fidelity lift and drag forces. Furthermore, an accurate six-degree-of-freedom dynamic model of the parafoil system is implemented based on the estimated coefficients. Simulations are conducted to prove the dynamic stability of the model and the feasibility of trajectory tracking. At last, simulation results of basic motions are compared with airdrop testing data, which demonstrates that the established model is capable of accurately predicting the flight behaviors of the parafoil system.
分类号	一类
资助项目	National Natural Science Foundation of China[61973172] ; National Natural Science Foundation of China[61973175] ; National Natural Science Foundation of China[62003175] ; National Natural Science Foundation of China[62003177] ; key Technologies Research and Development Program of Tianjin[19JC- ZDJC32800] ; China Postdoctoral Science Foundation[2020M670633] ; China Postdoctoral Science Foundation[2020M670045]
WOS关键词	PREDICTION
WOS研究方向	Engineering ; Mechanics
语种	英语
WOS记录号	WOS:000652940100004
资助机构	National Natural Science Foundation of China ; key Technologies Research and Development Program of Tianjin ; China Postdoctoral Science Foundation
其他责任者	Sun, Qinglin
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/86919]
专题	力学研究所_高温气体动力学国家重点实验室
作者单位	1.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China 2.China Aerosp Sci & Technol Corp, Lab Aerosp Entry Descent & Landing Technol, Beijing 100094, Peoples R China; 3.Beijing Inst Space Mech & Elect, Beijing 100094, Peoples R China; 4.Nankai Univ, Coll Artificial Intelligence, Tianjin 300350, Peoples R China;
推荐引用方式 GB/T 7714	Zhu, Hong,Sun, Qinglin,Liu, Xuefeng,et al. Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system[J]. NONLINEAR DYNAMICS,2021:22.
APA	Zhu, Hong.,Sun, Qinglin.,Liu, Xuefeng.,Liu, Jinglei.,Sun, Hao.,...&Chen, Zengqiang.(2021).Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system.NONLINEAR DYNAMICS,22.
MLA	Zhu, Hong,et al."Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system".NONLINEAR DYNAMICS (2021):22.