A thermo-mechanical coupling model for simulating the re-entry failure evolution mechanism of spacecraft propulsion module

Author:

Liu Zhihui,Li Zhihui,Ma Qiang

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference43 articles.

1. Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No. 1 spacecraft;Li;Adv. Aerodyn.,2019

2. Estimation of debris dispersion due to a space vehicle breakup during reentry;Reyhanoglu;Acta Astronaut.,2013

3. Simulation methods of aerodynamics covering various flow regimes and applications to aerodynamic characteristics of re-entry spacecraft module;Li;Acta Aerod. Sin.,2018

4. A novel nonlinear finite element method for structural dynamic modeling of spacecraft under large deformation;Ji;Thin-Walled Struct.,2021

5. Study on finite element algorithm for three dimensional transient heat transfer during falling reentry of spacecraft with metal truss structure;Shi;Chinese J. Comput. Mech.,2019

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Cellular gradient algorithm for solving complex mechanical optimization design problems;International Journal of Mechanical Sciences;2024-11

2. Large-scale sandwich structures optimization using Bayesian method;International Journal of Mechanical Sciences;2024-06

3. Numerical simulation of fatigue crack growth in an engine heat shield;Mechanics Based Design of Structures and Machines;2023-11-09

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3