Published May 1, 2018 | Version v1
Journal article

Comparative Analyses of Creep Models of a Solid Propellant

  • 1. 713 Research Institute of China Shipbuilding Industry Corporation, Zhengzhou, 450015 (China)

Description

The creep experiments of a solid propellant samples under five different stresses are carried out at 293.15 K and 323.15 K. In order to express the creep properties of this solid propellant, the viscoelastic model i.e. three Parameters solid, three Parameters fluid, four Parameters solid, four Parameters fluid and exponential model are involved. On the basis of the principle of least squares fitting, and different stress of all the parameters for the models, the nonlinear fitting procedure can be used to analyze the creep properties. The study shows that the four Parameters solid model can best express the behavior of creep properties of the propellant samples. However, the three Parameters solid and exponential model cannot very well reflect the initial value of the creep process, while the modified four Parameters models are found to agree well with the acceleration characteristics of the creep process. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/359/1/012050

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
359
Journal Issue
1
Journal Page Range
[5 p.]
ISSN
1757-899X

Conference

Title
International Conference on Computer Information and Automation Engineering
Dates
17-19 Nov 2017
Place
Yichang (China)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52091691
Subject category
S10: SYNTHETIC FUELS; S37: INORGANIC, ORGANIC, PHYSICAL AND ANALYTICAL CHEMISTRY;
Resource subtype / Literary indicator
Conference
Descriptors DEI
CREEP; EXPLOSIVES; FLUIDS; FUELS; LEAST SQUARE FIT; SOLIDS
Descriptors DEC
MATHEMATICAL SOLUTIONS; MAXIMUM-LIKELIHOOD FIT; MECHANICAL PROPERTIES; NUMERICAL SOLUTION