Comparative Analyses of Creep Models of a Solid Propellant
Creators
- 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/359/1/012050Additional details
Identifiers
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