Thermodynamic analysis and the recuperator’s effects on two cycle systems aiming for hypersonic vehicles-Reference-Cited by-同舟云学术

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Thermodynamic analysis and the recuperator’s effects on two cycle systems aiming for hypersonic vehicles

Published:2022-09 Issue: Volume:34 Page:101432
ISSN:2451-9049
Container-title:Thermal Science and Engineering Progress
language:en
Short-container-title:Thermal Science and Engineering Progress

Author:

Ma Yuan,Xie Gongnan,Manca Oronzio

Funder

Higher Education Discipline Innovation Project

National Natural Science Foundation of China

Science, Technology and Innovation Commission of Shenzhen Municipality

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes

Reference40 articles.

1. A century of ramjet propulsion technology evolution;Fry;J. Propul. Power,2004

2. Design and heat transfer characteristics analysis of combined active and passive thermal protection system for hydrogen fueled scramjet;Zhang;Int. J. Hydrogen Energy,2015

3. A review of regenerative cooling technologies for scramjets;Luo;Appl. Therm. Eng.,2021

4. Heat transfer of aviation kerosene at supercritical conditions;Zhong;AIAA J. Thermophys. Heat Transfer,2009

5. Hyper-X: Foundation for future hypersonic launch vehicles;McClinton;Acta Astronaut.,2005

Cited by 1 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. Investigation on the effect of the cooler design on the performance of onboard supercritical carbon dioxide power cycle for hypersonic vehicles;Applied Thermal Engineering;2024-01

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