Performance Evaluation of Hypersonic Pre-Cooled Turbojet Engine

Author:

Taguchi Hideyuki,Kobayashi Hiroaki,Kojima Takayuki,Hongoh Motoyuki,Masaki Daisaku,Nishida Shunsuke

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Experimental insights into thermal performance of a microtube precooler with drastic coolant properties variation and precooling impacts on turbojet engine operation;Energy;2023-09

2. Mach 4 Propulsive Performance Evaluation of Hypersonic Pre-Cooled Turbojet Engine;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10

3. Numerical Analysis on Supersonic Inlet Buzz;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2019

4. Mach 4 Performance Evaluation of Hypersonic Pre-Cooled Turbojet Engine;22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference;2018-09-15

5. Inter-Phase Momentum and Energy Transfer Effects of Nano-Aerosols on the Performance of Supersonic Intake Systems;2018 Joint Propulsion Conference;2018-07-08

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