Active flow control by a novel combinational active thermal protection for hypersonic vehicles-Reference-Cited by-同舟云学术

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Active flow control by a novel combinational active thermal protection for hypersonic vehicles

Published:2020-05 Issue: Volume:170 Page:320-330
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Huang Jie^ORCID,Yao Wei-Xing

Funder

National Postdoctoral Program for Innovative Talents

China Postdoctoral Science Foundation

Jiangsu Planned Projects for Postdoctoral Research Funds

Priority Academic Program Development of Jiangsu Higher Education Institutions

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles;Persova;Acta Astronaut.,2017

2. Validation of vibration-dissociation coupling models in hypersonic non-equilibrium separated flows;Shoev;Acta Astronaut.,2018

3. Thermal protection system gap analysis using a loosely coupled fluid-structural thermal numerical method;Huang;Acta Astronaut.,2018

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

5. Uncertainty dynamic theoretical analysis on ceramic thermal protection system using perturbation method;Huang;Acta Astronaut.,2018

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1. Optimization of MTI structure based on material characteristics under extreme aerodynamic heating environment;Thermal Science and Engineering Progress;2024-05

2. Numerical study for heat dissipation performance of phase transition cooling structure towards the wing antenna of hypersonic vehicle;Applied Thermal Engineering;2024-05

3. Study of the spike-aerodisk-opposing jet on heat protection to both the spike-aerodisk and the blunt body and overall drag reduction in rarefied hypersonic flow in near space;Aerospace Science and Technology;2024-04

4. Three-dimensional numerical study on reducing hypersonic blunt body drag and aeroheating with spike-aerodisk-bleed air channel;Acta Astronautica;2024-02

5. Anti-ablation properties of ZrB₂ modified carbon/phenolic composites in plasma wind tunnel;Journal of Composite Materials;2023-11-15

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