Heat reduction mechanism of hypersonic spiked blunt body with installation angle at large angle of attack-Reference-Cited by-同舟云学术

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Heat reduction mechanism of hypersonic spiked blunt body with installation angle at large angle of attack

Published:2019-11 Issue: Volume:164 Page:268-276
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Huang Jie,Yao Wei-Xing,Qin Ning

Funder

Priority Academic Program Development of Jiangsu Higher Education Institutions

National Postdoctoral Program for Innovative Talents

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 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. Nonablative lightweight thermal protection system for mars aeroflyby sample collection mission;Suzuki;Acta Astronaut.,2017

5. Parametric study on the drag and heat flux reduction mechanism of forward-facing cavity on a blunt body in supersonic flows;Huang;Aero. Sci. Technol.,2017

Cited by 12 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. Monotonicity-Based Interval Analysis Methods of Half-Wave Wall Radomes With Thickness and Permittivity Errors;IEEE Transactions on Antennas and Propagation;2022-12

2. Numerical study of reverse jet for mitigating shock/shock interaction heating;Aerospace Science and Technology;2022-12

3. Effect of spike geometry on hemispherical blunt body;INTERNATIONAL CONFERENCE ON ADVANCES IN MULTI-DISCIPLINARY SCIENCES AND ENGINEERING RESEARCH: ICAMSER-2021;2022

4. Coupled Fluid-Thermal Investigation on Drag and Heat Reduction of a Hypersonic Spiked Blunt Body with an Aerodisk;Aerospace;2021-12-30

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

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