Refined Bird Model Considering Soft and Skeletal Tissues for Bird Impact SimulationSource: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006::page 04024072-1DOI: 10.1061/JAEEEZ.ASENG-5417Publisher: American Society of Civil Engineers
Abstract: To more accurately characterize the load characteristics of birds under the impact of aviation structures, this study conducted computed tomography scanning of a 1-kg chicken and proposed a geometric model of the bird, including bones, muscles, viscera, and cavities. The constitutive model of fluid dynamics was used to describe the rheological properties of muscle viscera, and a bilinear follow-up plastic model with failure was proposed to describe the mechanical behavior of bones under high-speed impact, and then the bone and muscle/viscera models were assembled into a refined bird model to establish a finite element model. The model was verified with bird impact testing on a rigid target. By comparing and analyzing the impact pressure with the traditional bird model, it was found that the initial impact pressure and stagnation flow pressure of the CT scan refined bird model were lower than those of the traditional bird model and were close to the experimental values. The reason for this phenomenon is that the CT scan refined bird model to some extent reproduces the response of the real structure inside the bird body during the impact process, the high strength level of the bone part model will reduce the material’s movement speed after the bird body model rheological changes, and it well demonstrates the phenomenon of reduced mixing density after rheological deformation during simulation.
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contributor author | Gang Luo | |
contributor author | Mingyu Wang | |
contributor author | Fengqi Zhang | |
contributor author | Haiyang Zhang | |
contributor author | Lulu Liu | |
contributor author | Wei Chen | |
date accessioned | 2024-12-24T10:14:35Z | |
date available | 2024-12-24T10:14:35Z | |
date copyright | 11/1/2024 12:00:00 AM | |
date issued | 2024 | |
identifier other | JAEEEZ.ASENG-5417.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4298558 | |
description abstract | To more accurately characterize the load characteristics of birds under the impact of aviation structures, this study conducted computed tomography scanning of a 1-kg chicken and proposed a geometric model of the bird, including bones, muscles, viscera, and cavities. The constitutive model of fluid dynamics was used to describe the rheological properties of muscle viscera, and a bilinear follow-up plastic model with failure was proposed to describe the mechanical behavior of bones under high-speed impact, and then the bone and muscle/viscera models were assembled into a refined bird model to establish a finite element model. The model was verified with bird impact testing on a rigid target. By comparing and analyzing the impact pressure with the traditional bird model, it was found that the initial impact pressure and stagnation flow pressure of the CT scan refined bird model were lower than those of the traditional bird model and were close to the experimental values. The reason for this phenomenon is that the CT scan refined bird model to some extent reproduces the response of the real structure inside the bird body during the impact process, the high strength level of the bone part model will reduce the material’s movement speed after the bird body model rheological changes, and it well demonstrates the phenomenon of reduced mixing density after rheological deformation during simulation. | |
publisher | American Society of Civil Engineers | |
title | Refined Bird Model Considering Soft and Skeletal Tissues for Bird Impact Simulation | |
type | Journal Article | |
journal volume | 37 | |
journal issue | 6 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/JAEEEZ.ASENG-5417 | |
journal fristpage | 04024072-1 | |
journal lastpage | 04024072-11 | |
page | 11 | |
tree | Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006 | |
contenttype | Fulltext |