• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利：CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法，用中文像聊天一样搜索，搜遍4000万医学文献。AI智能推荐，让科研检索更轻松。

立即免费搜索

文件翻译

保留排版，准确专业，支持PDF/Word/PPT等文件格式，支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述，25分钟生成高质量综述，智能提取关键信息，辅助科研写作。

立即免费体验

一种用于研究航空航天材料在无控大气再入过程中响应行为的快速热一维模型。

A Fast Thermal 1D Model to Study Aerospace Material Response Behaviors in Uncontrolled Atmospheric Entries.

作者信息

Pirrone Serena R M, Agabiti Camilla, Pagan Adam S, Herdrich Georg

机构信息

Bioinspired Soft Robotics Laboratory, Istituto Italiano di Tecnologia (IIT), Via Morego 30, 16163 Genova, Italy.

The BioRobotics Institute, Scuola Superiore Sant'Anna, Viale Rinaldo Piaggio 34, 56025 Pontedera, Italy.

出版信息

Materials (Basel). 2022 Feb 17;15(4):1505. doi: 10.3390/ma15041505.

DOI:10.3390/ma15041505
PMID:35208044
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC8875084/
Abstract

A preliminary thermal 1D numerical model for studying the demise behavior of stainless steel 316L, silicon carbide (SiC) and carbon fiber reinforced polymer (CFRP) during uncontrolled atmospheric entry is proposed. Test case modeling results are compared to experimental data obtained in the framework of ESA Clean Space initiative: material samples were exposed to different heat flux conditions using the Plasma Wind Tunnel (PWT) facilities at the Institute of Space Systems (IRS) of the University of Stuttgart. This numerical model approximates the heating history of the selected materials by simulating their thermal response and temperature profiles, which have trends similar to the experimental curves that are found. Moreover, when high heat flux conditions are considered, the model simulates the materials' mass loss due to the ablation process: at the end of the simulation, the difference between the experimental and the modeled results is about 17% for CFRP and 35% for stainless steel. To reduce the model's uncertainties, the following analysis suggests the need to consider the influence of adequate material thermophysical properties and the physical-chemical processes that affect the samples' temperature profile and mass loss.

摘要

提出了一个初步的一维热数值模型，用于研究316L不锈钢、碳化硅（SiC）和碳纤维增强聚合物（CFRP）在非受控大气再入过程中的烧蚀行为。将测试案例建模结果与在欧洲航天局清洁空间倡议框架下获得的实验数据进行了比较：使用斯图加特大学空间系统研究所（IRS）的等离子风洞（PWT）设施，将材料样本暴露于不同的热流条件下。该数值模型通过模拟所选材料的热响应和温度分布来近似其加热历史，这些热响应和温度分布具有与所发现的实验曲线相似的趋势。此外，当考虑高热流条件时，该模型模拟了由于烧蚀过程导致的材料质量损失：在模拟结束时，CFRP的实验结果与建模结果之间的差异约为17%，不锈钢的差异约为35%。为了减少模型的不确定性，以下分析表明需要考虑适当的材料热物理性质以及影响样本温度分布和质量损失的物理化学过程的影响。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/ce98a6368ebc/materials-15-01505-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/64c853b2ef6d/materials-15-01505-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/1ebce1f6f6a0/materials-15-01505-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/4652b5a50ef2/materials-15-01505-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/585b3d2f2acd/materials-15-01505-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/7dde206091f4/materials-15-01505-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/e7162f8d3e8a/materials-15-01505-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/87a5522762b6/materials-15-01505-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/a1db4a6a94ea/materials-15-01505-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/0e1cb2ac93bc/materials-15-01505-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/087d5a27c687/materials-15-01505-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/e355c155495b/materials-15-01505-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/f4ebc6e20912/materials-15-01505-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/ce98a6368ebc/materials-15-01505-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/64c853b2ef6d/materials-15-01505-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/1ebce1f6f6a0/materials-15-01505-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/4652b5a50ef2/materials-15-01505-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/585b3d2f2acd/materials-15-01505-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/7dde206091f4/materials-15-01505-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/e7162f8d3e8a/materials-15-01505-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/87a5522762b6/materials-15-01505-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/a1db4a6a94ea/materials-15-01505-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/0e1cb2ac93bc/materials-15-01505-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/087d5a27c687/materials-15-01505-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/e355c155495b/materials-15-01505-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/f4ebc6e20912/materials-15-01505-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/cffc/8875084/ce98a6368ebc/materials-15-01505-g013.jpg

相似文献

1
A Fast Thermal 1D Model to Study Aerospace Material Response Behaviors in Uncontrolled Atmospheric Entries.一种用于研究航空航天材料在无控大气再入过程中响应行为的快速热一维模型。
Materials (Basel). 2022 Feb 17;15(4):1505. doi: 10.3390/ma15041505.
2
Thermo-elastic behaviour of carbon-fiber reinforced polymer and the effect of adding nanoparticles at elevated heat intensity.碳纤维增强聚合物的热弹性行为以及在高热强度下添加纳米颗粒的影响。
Heliyon. 2020 Mar 30;6(3):e03622. doi: 10.1016/j.heliyon.2020.e03622. eCollection 2020 Mar.
3
An open carbon-phenolic ablator for scientific exploration.一种用于科学探索的开放式碳酚醛烧蚀材料。
Sci Rep. 2023 Aug 12;13(1):13135. doi: 10.1038/s41598-023-40351-x.
4
Measurements of thermophysical properties of solid and liquid NIST SRM 316L stainless steel.固体和液体NIST SRM 316L不锈钢热物理性质的测量。
J Mater Sci. 2020;55. doi: 10.1007/s10853-019-04261-6.
5
Instantaneous Ablation Behavior of Laminated CFRP by High-Power Continuous-Wave Laser Irradiation in Supersonic Wind Tunnel.高功率连续波激光在超音速风洞中辐照层压碳纤维增强塑料的瞬态烧蚀行为
Materials (Basel). 2023 Jan 13;16(2):790. doi: 10.3390/ma16020790.
6
Study of Polymer Matrix Degradation Behavior in CFRP Short Pulsed Laser Processing.碳纤维增强塑料短脉冲激光加工中聚合物基体降解行为的研究
Polymers (Basel). 2016 Aug 15;8(8):299. doi: 10.3390/polym8080299.
7
A Constitutive Model of High-Early-Strength Cement with Perlite Powder as a Thermal-Insulating Material Confined by Caron Fiber Reinforced Plastics at Elevated Temperatures.以珍珠岩粉为保温材料、采用碳纤维增强塑料约束的高温下早强水泥本构模型
Polymers (Basel). 2020 Oct 15;12(10):2369. doi: 10.3390/polym12102369.
8
Effect of Temperature on Material Properties of Carbon Fiber Reinforced Polymer (CFRP) Tendons: Experiments and Model Assessment.温度对碳纤维增强聚合物（CFRP）筋材材料性能的影响：试验与模型评估
Materials (Basel). 2019 Mar 28;12(7):1025. doi: 10.3390/ma12071025.
9
Thermal Ablation Damage Analysis of CFRP Suffering from Lightning Based on Principles of Tomography.基于层析成像原理的碳纤维增强复合材料雷击热烧蚀损伤分析
Materials (Basel). 2020 Nov 16;13(22):5159. doi: 10.3390/ma13225159.
10
A Novel Strengthening Method for Damaged Pipeline under High Temperature Using Inorganic Insulation Material and Carbon Fiber Reinforced Plastic Composite Material.一种利用无机保温材料和碳纤维增强塑料复合材料对高温下受损管道的新型加固方法。
Materials (Basel). 2019 Oct 24;12(21):3484. doi: 10.3390/ma12213484.

引用本文的文献

1
Thermal Behavior of Carbon-Phenolic/Silica Phenolic Dual-Layer Ablator Specimens through Arc-Jet Tests.通过电弧喷射试验研究碳酚醛/二氧化硅酚醛双层烧蚀材料试样的热行为
Materials (Basel). 2023 Aug 30;16(17):5929. doi: 10.3390/ma16175929.

本文引用的文献

1
Modelling Behaviour of a Carbon Epoxy Composite Exposed to Fire: Part II-Comparison with Experimental Results.碳环氧复合材料在火灾中的行为建模：第二部分——与实验结果的比较
Materials (Basel). 2017 Apr 28;10(5):470. doi: 10.3390/ma10050470.