Simulation Analysis for Deformation and Performance Evolution of Aerospace Composite Tank During Curing Process

Author:

Guan Chenglong1ORCID,Chen Junhao1ORCID,Zhan Lihua2ORCID,Chi Tongming1ORCID,Wang Bing1ORCID,Zhong Shuncong1ORCID

Affiliation:

1. Fujian Provincial Key Laboratory of Terahertz Functional Devices and Intelligent Sensing, School of Mechanical Engineering and Automation, Fuzhou University, China

2. State Key Laboratory of Precision Manufacturing for Extreme Service Performance, Central South University, China

Funder

Fujian Provincial Major Research Project

Fuzhou University

National Natural Science Foundation of China

Publisher

ACM

Reference13 articles.

1. Progress in research on composite cryogenic propellant tank for large aerospace vehicles[J];Liu N;Composites Part A-Applied Science and Manufacturing,2021

2. Research and application progress of key technologies for composites cryogenic tanks[J];Wu Z;Aeronautical Manufacturing Technology,2021

3. Mathematical modeling of thermal stratification in a double wall cryogenic propellant tank with different insulations using one-dimensional flow over vertical plate approximation[J];Vishnu S B;Cryogenics,2022

4. Gas permeation of composites subjected to impact for cryogenic applications[J];Flanagan M;Journal of Spacecraft and Rockets,2022

5. Permeability of carbon fibre PEEK composites for cryogenic storage tanks of future space launchers[J];Flanagan M;Composites Part A-Applied Science and Manufacturing,2017

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