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Component-based CMDB propellant mechanical prediction method

A technology of propellant and mechanics, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of model parameter acquisition relying on experimental data, gap between model prediction and actual demand, and insufficient systematic and in-depth research

Inactive Publication Date: 2018-11-16
BEIJING INSTITUTE OF TECHNOLOGYGY
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Problems solved by technology

[0003] To sum up, there are currently many studies on the macroscopic laws of its mechanical properties, and most of the established mechanical models are macroscopic empirical models. The prediction results of these models are in good agreement with the experimental results, but the acquisition of model parameters is highly dependent on Experimental data, and the research on revealing the nature of regular changes, the influence of component composition on stress-strain curve and stress-strain energy, component microstructure and the correlation between adhesive matrix network structure and mechanical properties is not systematic enough. And in-depth, lack of theoretical models at the micro level, there is still a big gap between the prediction of the model and the actual demand

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  • Component-based CMDB propellant mechanical prediction method
  • Component-based CMDB propellant mechanical prediction method
  • Component-based CMDB propellant mechanical prediction method

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Embodiment 1

[0082] In order to verify the feasibility of the method, the mass fractions of the selected CMDB propellant components are: 50% nitrocellulose NC (12.5% ​​nitrogen content), 32% NG, 10% Octogen HMX, and the remaining additives 8%.

[0083] like figure 1 As shown, a component-based CMDB propellant mechanics prediction method disclosed in this embodiment includes the following steps:

[0084] Step 1: Select and obtain the input parameters of the components according to the atomic group contribution and selection principle table.

[0085] Obtain the molecular degree of freedom N and zero-point binding energy E of the chemical bond by looking up the contribution of the atomic group and the selection principle table coh , and the van der Waals volume V w . According to the principle of superposition, the molecular degree of freedom N=61.3 and the zero-point binding energy E of nitrocellulose NC in CMDB propellant can be respectively determined coh =235070J / mol, and van der Waals...

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Abstract

The invention discloses a component-based CMDB propellant mechanical prediction method, relates to a mechanical property prediction method at a wide strain rate, is applicable to the field of CMDB propellant formula mechanical optimization design, and belongs to the field of solid propellant rate dependence mechanical properties. The implementation method comprises the following steps that according to atomic group contribution and selection principle, input parameters obtaining components are selected, a potential-energy function of an adhesive matrix is built, and by quantizing storage modulus and Young modulus, the glass-transition temperature and the Young modulus of the adhesive matrix of a CMDB propellant are calculated. Considering the solid particle strengthening effect, the Youngmodulus of the CMDB propellant is calculated; a rate dependence constitutive model is built through integration; the rate dependence constitutive model can be applied to application fields related tothe CMDB propellant, prediction of the relation between the CMDB propellant molecular structure and the mechanical property is achieved, and engineering problems in the application fields related to the CMDB propellant are solved.

Description

technical field [0001] The invention relates to a component-based CMDB propellant mechanical prediction method, in particular to a mechanical performance prediction method under a wide strain rate, which is applicable to the field of mechanical optimization design of CMDB propellant formula and belongs to the field of solid propellant rate-dependent mechanical properties . Background technique [0002] A solid propellant is a nonlinear viscoelastic material. At present, there are multiple integral nonlinear constitutive models and single integral nonlinear constitutive models to describe the nonlinear mechanical behavior of materials. Compared with the multi-integral nonlinear constitutive model, the single-integral nonlinear constitutive model is simple in form and has fewer parameters, which is convenient for secondary development of finite element software and has been widely used in engineering. Common single-integral nonlinear constitutive models include Leaderman con...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F2119/08G06F2119/06G06F30/20
Inventor 周海霞谢侃李世鹏隋欣白龙王宁飞
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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