Phase transition cooling structure towards the wing antenna of hypersonic vehicle-Reference-Cited by-同舟云学术

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Phase transition cooling structure towards the wing antenna of hypersonic vehicle

Published:2024-03 Issue: Volume:197 Page:108844
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Jin Hua,Li Zhuoran,Wu Xiao,Hu Feng,Luo Xianlong,Zhang Jieyan

Funder

National Key Laboratory of Science, Technology on Advanced Composites in Special Environments, HIT

National Natural Science Foundation of China

National Key Laboratory Foundation of China

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference31 articles.

1. Numerical investigation on the characteristics of cavity-transpiration combined cooling for hypersonic vehicle leading edge;Wang;Appl. Therm. Eng.,2023

2. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles;Zhu;Chin. J. Aeronaut.,2018

3. Review of control and guidance technology on hypersonic vehicle;Ding;Chin. J. Aeronaut.,2022

4. Model predictive based unscented kalman filter for hypersonic vehicle navigation with INS/GNSS integration;Hu;IEEE Access,2020

5. Terminal guidance for a hypersonic vehicle with impact time control;Wang;J. Guid. Control Dynam.,2018

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1. Numerical investigation of blunt body's resistance and heat reduction with combination of airway spike and root jet;International Journal of Thermal Sciences;2024-09

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