Numerical Simulation of the Impact of A320 on Rigid Target and Determination of the Correction Coefficient α in the Modified Riera Model

Li Jing Wen; Chun Ming Zhang; Chao Guo; Yu Gao; Pu Duan; Zhuo Cheng Ou; Zhuo Ping Duan

Numerical Simulation of the Impact of A320 on Rigid Target and Determination of the Correction Coefficient α in the Modified Riera Model

Li Jing Wen, Chun Ming Zhang, Chao Guo, Yu Gao, Pu Duan, Zhuo Cheng Ou, Zhuo Ping Duan^*

^*此作品的通讯作者

机电学院

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The impact processes of an Airbus A320 airplane upon a rigid target under different impact velocities and different impact angles are simulated by using the general explicit dynamic analysis program LS-DYNA. Through comparing the numerical simulation results of the impact loads with the calculated results of the modified Riera impact load equation, the correction coefficient α in the modified Riera impact load equation under different impact velocities are determined. It is showed that the correction coefficient α is not a constant, moreover, there is a linear relationship between α and the square of the impact velocity V₀². The impact loads calculated with the modified Riera impact load equation are in good agreement with the numerical simulation results, which verifies the rationality of the modified Riera model.

源语言	英语
页（从-至）	51-56
页数	6
期刊	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
卷	37
出版状态	已出版 - 1 12月 2017

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title = "Numerical Simulation of the Impact of A320 on Rigid Target and Determination of the Correction Coefficient α in the Modified Riera Model",

abstract = "The impact processes of an Airbus A320 airplane upon a rigid target under different impact velocities and different impact angles are simulated by using the general explicit dynamic analysis program LS-DYNA. Through comparing the numerical simulation results of the impact loads with the calculated results of the modified Riera impact load equation, the correction coefficient α in the modified Riera impact load equation under different impact velocities are determined. It is showed that the correction coefficient α is not a constant, moreover, there is a linear relationship between α and the square of the impact velocity V02. The impact loads calculated with the modified Riera impact load equation are in good agreement with the numerical simulation results, which verifies the rationality of the modified Riera model.",

keywords = "Aircraft impact, Impact load, Numerical simulation, Riera model",

author = "Wen, {Li Jing} and Zhang, {Chun Ming} and Chao Guo and Yu Gao and Pu Duan and Ou, {Zhuo Cheng} and Duan, {Zhuo Ping}",

year = "2017",

month = dec,

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language = "English",

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journal = "Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology",

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TY - JOUR

T1 - Numerical Simulation of the Impact of A320 on Rigid Target and Determination of the Correction Coefficient α in the Modified Riera Model

AU - Wen, Li Jing

AU - Zhang, Chun Ming

AU - Guo, Chao

AU - Gao, Yu

AU - Duan, Pu

AU - Ou, Zhuo Cheng

AU - Duan, Zhuo Ping

PY - 2017/12/1

Y1 - 2017/12/1

N2 - The impact processes of an Airbus A320 airplane upon a rigid target under different impact velocities and different impact angles are simulated by using the general explicit dynamic analysis program LS-DYNA. Through comparing the numerical simulation results of the impact loads with the calculated results of the modified Riera impact load equation, the correction coefficient α in the modified Riera impact load equation under different impact velocities are determined. It is showed that the correction coefficient α is not a constant, moreover, there is a linear relationship between α and the square of the impact velocity V02. The impact loads calculated with the modified Riera impact load equation are in good agreement with the numerical simulation results, which verifies the rationality of the modified Riera model.

AB - The impact processes of an Airbus A320 airplane upon a rigid target under different impact velocities and different impact angles are simulated by using the general explicit dynamic analysis program LS-DYNA. Through comparing the numerical simulation results of the impact loads with the calculated results of the modified Riera impact load equation, the correction coefficient α in the modified Riera impact load equation under different impact velocities are determined. It is showed that the correction coefficient α is not a constant, moreover, there is a linear relationship between α and the square of the impact velocity V02. The impact loads calculated with the modified Riera impact load equation are in good agreement with the numerical simulation results, which verifies the rationality of the modified Riera model.

KW - Aircraft impact

KW - Impact load

KW - Numerical simulation

KW - Riera model

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M3 - Article

AN - SCOPUS:85047213264

SN - 1001-0645

VL - 37

SP - 51

EP - 56

JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

JF - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

ER -

Numerical Simulation of the Impact of A320 on Rigid Target and Determination of the Correction Coefficient α in the Modified Riera Model

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