Heat reduction mechanism and aerodynamic optimization of combined non-ablative thermal protection system concept-Reference-Cited by-同舟云学术

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Heat reduction mechanism and aerodynamic optimization of combined non-ablative thermal protection system concept

Published:2020-05 Issue: Volume:152 Page:119549
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Huang Jie,Yao Wei-Xing

Funder

National Postdoctoral Program

China Postdoctoral Science Foundation

Jiangsu Planned Projects for Postdoctoral Research Funds

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference40 articles.

1. Thermal protection systems in spacecraft re-entry-a brief overview;Zheng;Int. J. Heat Mass Tran.,2013

2. Coupled heat transfer and thermo-mechanical behavior of hypersonic cylindrical leading edges;Chen;Int. J. Heat Mass Tran.,2018

3. Thermal force and moment determination of an integrated thermal protection system;Oscar;AIAA J.,2010

4. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream;Mair;Philos. Mag.,1952

5. Hypersonic flow over axially symmetric spiked bodies;Maull;J. Fluid Mech.,1960

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1. Lightweight nitrogen‐doped phenolic composites with enhanced thermal ablation‐insulation performance by improving pyrolysis gas blocking effect;Polymer Composites;2023-12-22

2. Aerothermal effects of ablation on carbon-based space objects;International Journal of Heat and Mass Transfer;2023-03

3. Components of thermal protection mechanism of carbon/phenolic composites exposed to severe aerodynamic heat;Polymer Composites;2022-09-07

4. Three-dimensional numerical study of the directional heat transfer in an L-shaped carbon/carbon composite thermal protection system;International Journal of Thermal Sciences;2021-10

5. Optimization of multilayer thermal protection system by using phase change material under aerodynamic heating;Applied Thermal Engineering;2021-06

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