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Occupant’s lower extremities’ impact-based model calibration for vehicle under-belly blast

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Abstract

Computer-aided engineering (CAE) technology is an important tool in the research of vehicle under-belly blast. A high-quality CAE model is required to guarantee accurate prediction. This requires an efficient model calibration process with physical testing, but the traditional model calibration method based on trial and error and operators’ experience is usually very inefficient and arbitrary. In this paper, an automatic model calibration process based on the Error Assessment of Response Time Histories (EARTH) metric is applied. The EARTH metric evaluates the discrepancies between test and CAE by quantifying the phase error, magnitude error, and slope error between their time histories. Then, an automatic calibration process can be achieved by solving a multi-objective optimization problem for which the optimization object is minimizing discrepancies between testing and CAE and results in automatic calibration of key parameters of the blast simulation CAE model. A case of occupant’s lower extremities’ responses under vehicle under-belly blast load is studied as an example to demonstrate the feasibility of the applied method.

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Data availability

Keyword files and test data files are not available. DOE used for multi-objective optimization is available.

Abbreviations

A :

Constant parameter in JWL equation

A i :

Face area of ALE element

B :

Constant parameter in JWL equation

d DTW :

DTW distance

d i :

Penetration distance

d[i, j]:

Cost matrix

D[i, j]:

Cumulative cost matrix

E 0 :

Specific internal energy in JWL equation

\( \overline{\varepsilon} \) :

Average error

ε m :

Magnitude error

ε p :

Phase error

ε s :

Slope error

\( {\overline{\varepsilon}}_{\mathrm{p}} \) :

Average phase error

\( {\overline{\varepsilon}}_{\mathrm{m}} \) :

Average magnitude error

\( {\overline{\varepsilon}}_{\mathrm{s}} \) :

Average slope error

\( {\overline{\varepsilon}}_{\mathrm{p},\mathrm{b}} \) :

Average phase error of baseline model

\( {\overline{\varepsilon}}_{\mathrm{m},\mathrm{b}} \) :

Average magnitude error of baseline model

\( {\overline{\varepsilon}}_{\mathrm{s},\mathrm{b}} \) :

Average slope error of baseline model

\( {\overline{\varepsilon}}_{\mathrm{p},\mathrm{nor}} \) :

Normalized average phase error

\( {\overline{\varepsilon}}_{\mathrm{m},\mathrm{nor}} \) :

Normalized average magnitude error

\( {\overline{\varepsilon}}_{\mathrm{s},\mathrm{nor}} \) :

Normalized average slope error

\( {\overline{\varepsilon}}_{\mathrm{overall}} \) :

Overall error

f si :

Scale factor for interface spring stiffness

F i :

Interface force

h :

Minimum sampling time step of data

k i :

Stiffness of interface spring

K i :

Bulk modulus of ALE element

n c :

Value for maximum cross-correlation

p :

Pressure of blast gas in JWL equation

\( \overline{R} \) :

Average residual

R 1 :

Constant parameter in JWL equation

R 2 :

Constant parameter in JWL equation

r(n):

Cross-correlation

ρ :

Correlation coefficient

SS :

Sum of squares

σ R :

Standard deviation of residual

t′:

Minimum time interval (ms)

V :

Volume fraction of blast gas in JWL equation

V i :

Volume of ALE element

w k :

kth element of warping sequence

w K :

End point of warping sequence

W :

Warping sequence

ω :

Constant parameter in JWL equation

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Acknowledgments

The authors would like to acknowledge the Nanjing University of Science and Technology (NJUST) Vehicle Engineering Institute for the test and equipment support and the LetPub for its linguistic assistance during the preparation of this manuscript.

Funding

This work was supported by the National Natural Science Foundation of China (grant number 51405232).

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Correspondence to Xianhui Wang.

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The authors declare that they have no conflict of interest.

Code availability

MATLAB codes for calculations are available.

Replication of results

The authors cannot provide the keyword files for FEA and detail physical test data because of their confidentiality. So, the results presented in this paper cannot be reproduced perfectly. However, the readers can still replicate the calibration process with your own research object in similar area with codes for calculation available.

For software using, FEM was conducted by Hypermesh 2017; FEA was conducted by LS-Dyna with solver version R11; multi-objective optimization solving was conducted by ISight 2017; other calculations were conducted by MATLAB 2018b (MathWorks 2016). The DOE used for multi-objective optimization and the codes for calculation are available.

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Responsible editor: Raphael Haftka

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Zheng, Q., Wei, R., Li, M. et al. Occupant’s lower extremities’ impact-based model calibration for vehicle under-belly blast. Struct Multidisc Optim 63, 391–405 (2021). https://doi.org/10.1007/s00158-020-02668-3

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