Research of the dynamic load test in cylindrical structures

Li Jing Wen; Zhuo Ping Duan; Qiang Wang; Chao Guo; Ze Jian Xu; Feng Lei Huang

doi:10.15918/j.tbit1001-0645.2016.Suppl.1.031

Research of the dynamic load test in cylindrical structures

Li Jing Wen, Zhuo Ping Duan^*, Qiang Wang, Chao Guo, Ze Jian Xu, Feng Lei Huang

^*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

To accurately estimate the impact load in the experiment of large aircraft model hitting the concrete target, the test system of the small size of the cylindrical structures hitting the moving target was established. The decreasing acceleration curve of cylindrical structures was measured. Combined with linear density distribution, the impact load curve can be calculated. Compared with the experimental impact load curve, the results of theoretical calculation was verified and the theoretical calculation formula was improved.

源语言	英语
页（从-至）	123-126
页数	4
期刊	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
卷	36
DOI	https://doi.org/10.15918/j.tbit1001-0645.2016.Suppl.1.031
出版状态	已出版 - 1 6月 2016

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title = "Research of the dynamic load test in cylindrical structures",

abstract = "To accurately estimate the impact load in the experiment of large aircraft model hitting the concrete target, the test system of the small size of the cylindrical structures hitting the moving target was established. The decreasing acceleration curve of cylindrical structures was measured. Combined with linear density distribution, the impact load curve can be calculated. Compared with the experimental impact load curve, the results of theoretical calculation was verified and the theoretical calculation formula was improved.",

keywords = "Crippling force, Impact load, Linear density, Theoretical calculation",

author = "Wen, {Li Jing} and Duan, {Zhuo Ping} and Qiang Wang and Chao Guo and Xu, {Ze Jian} and Huang, {Feng Lei}",

year = "2016",

month = jun,

day = "1",

doi = "10.15918/j.tbit1001-0645.2016.Suppl.1.031",

language = "English",

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AU - Wen, Li Jing

AU - Duan, Zhuo Ping

AU - Wang, Qiang

AU - Guo, Chao

AU - Xu, Ze Jian

AU - Huang, Feng Lei

PY - 2016/6/1

Y1 - 2016/6/1

N2 - To accurately estimate the impact load in the experiment of large aircraft model hitting the concrete target, the test system of the small size of the cylindrical structures hitting the moving target was established. The decreasing acceleration curve of cylindrical structures was measured. Combined with linear density distribution, the impact load curve can be calculated. Compared with the experimental impact load curve, the results of theoretical calculation was verified and the theoretical calculation formula was improved.

AB - To accurately estimate the impact load in the experiment of large aircraft model hitting the concrete target, the test system of the small size of the cylindrical structures hitting the moving target was established. The decreasing acceleration curve of cylindrical structures was measured. Combined with linear density distribution, the impact load curve can be calculated. Compared with the experimental impact load curve, the results of theoretical calculation was verified and the theoretical calculation formula was improved.

KW - Crippling force

KW - Impact load

KW - Linear density

KW - Theoretical calculation

UR - http://www.scopus.com/inward/record.url?scp=84992179602&partnerID=8YFLogxK

U2 - 10.15918/j.tbit1001-0645.2016.Suppl.1.031

DO - 10.15918/j.tbit1001-0645.2016.Suppl.1.031

M3 - Article

AN - SCOPUS:84992179602

SN - 1001-0645

VL - 36

SP - 123

EP - 126

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

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

ER -

Research of the dynamic load test in cylindrical structures

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