Blind image separation for the debonding defects recognition of the solid propellant rocket motor cladding layer using pulse thermography-Reference-Cited by-同舟云学术

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Blind image separation for the debonding defects recognition of the solid propellant rocket motor cladding layer using pulse thermography

Published:2021-04 Issue: Volume:174 Page:108997
ISSN:0263-2241
Container-title:Measurement
language:en
Short-container-title:Measurement

Author:

Wang Fei,Liu Junyan,Dong Boyuan,Gong Jinlong,Peng Wei,Wang Yang,Chen Mingjun,Liu Guobin

Funder

Heilongjiang Provincial Postdoctoral Science Foundation

Foundation for Innovative Research Groups of the National Natural Science Foundation of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference44 articles.

1. Fatigue crack propagation behavior of carboxyl-terminated polybutadiene solid rocket propellants;López;Int. J. Fracture,2020

2. Sensitivity analysis and uncertainty quantification on aluminum particle combustion for an upward burning solid rocket propellant;Griego;Fuel,2019

3. Structural assessment of a solid propellant rocket motor: Effects of aging and damage;Yildinm;Aerosp. Sci. Technol.,2011

4. Analysis of aluminum particle combustion in a downward burning solid rocket propellant;Griego;Fuel,2019

5. Recent process of coating technologies for solid propellant;Bian;Chin. J. Explosives Propellants,2019

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