Experimental and Numerical Analysis of Pressure-Effect Threat Model Based on SPH Method-Reference-Cited by-同舟云学术

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Experimental and Numerical Analysis of Pressure-Effect Threat Model Based on SPH Method

Published:2022-05 Issue:3 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wu Xiaoyang¹,Chen Qing²,Zhang Ke³,Wang Peiyan⁴,Yue Zhufeng⁵

Affiliation:

1. Ph.D. Student, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.

2. Master’s Degree Candidate, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.

3. School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China (corresponding author).

4. Associate Professor, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.

5. Professor, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical Univ., Xi’an 710100, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001421

Reference25 articles.

1. Impact Simulation With an Aircraft Wing Using SPH Bird Model

2. On the structural stability of the Euler–Voigt and Navier–Stokes–Voigt models

3. Experiments and finite element simulations of a tyre blow-out process

4. A high-order SPH method by introducing inverse kernels

5. Development of a detailed aircraft tyre finite element model for safety assessment

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