首页|Fluid-structure interaction simulation for multi-body flexible morphing structures

Fluid-structure interaction simulation for multi-body flexible morphing structures

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The multi-body flexible morphing airfoil can improve the aerodynamic characteristics based on different flight missions continuously.Recently researches have focused on the unsteady aerodynamic characteristics of flexible wings under passive actuation.However,the unsteady aero-dynamic characteristics with the fluid-structure interaction effects in the multi-body active actua-tion process of morphing airfoil deserve further investigation.In this paper,a fluid-structure coupled simulation method for multi-body flexible morphing airfoil with active actuation subsystem was investigated,and the aerodynamic characteristics during deformation were compared with dif-ferent skin flexibility,flow field environment,actuation mode and actuation time.The numerical results show that for the steady aerodynamic,the skin flexibility can improve the stability efficiency.In the unsteady process,the change trend of the transient lift coefficient and pitching moment are consistent with those of the active drive characteristics,while the instantaneous lift-drag ratio coef-ficient is greatly affected by the driving mode and can be improved by increasing the driving dura-tion.

Fluid-structure interactionMulti-body dynamics mod-elingFlexible structuresAerodynamicsMorphing wings

Wenzhi GUO、Yongtao SHUI、Lu NIE、Gang CHEN

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State Key Laboratory of Strength and Vibration for Mechanic Structures,School of Aerospace Engineering,Xi'an Jiaotong University,Xi'an 710049,China

China Academy of Launch Vehicle Technology,Beijing 100076,China

China Academy of Aerospace Science and Innovation,Beijing 100086,China

Shannxi Key Laboratory of Service Environment and Control for Flight Vehicles,Xi'an Jiaotong Universitv,Xi'an 710049,China

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National Natural Science Foundation of ChinaNational Natural Science Foundation of ChinaNatural Science Foundation of Shaanxi Province,China

52192633118722932022JC-03

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(2)
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