Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network-Reference-Cited by-同舟云学术

Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network

Published:2019-05 Issue:5 Volume:32 Page:1059-1070
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LIU Menglong^ORCID,WANG Qiang,ZHANG Qingming,LONG Renrong,CUI Fangsen^ORCID,SU Zhongqing

Funder

Institute of High Performance Computing

Hong Kong Research Grants Council

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference28 articles.

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3. Office NODP. Monthly number of objects in Earth orbit by object type. Orbital Debris Quarterly News 2016; 20(1-2): 13-13

4. Kumar SKS, Jurado-Manriquez EA, Kim YH, Choi C, Baluch AH, Kim CG. Polybenzimidazole (PBI) film coating for improved hypervelocity impact energy absorption for space applications. Compos Struct. 2018;188: 72–7.

5. Voillat R, Gallien F, Mortensen A, Gass V. Hypervelocity impact testing on stochastic and structured open porosity cast Al-Si cellular structures for space applications. Int J Impact Eng. 2018, 120:126–37.

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