Research and Development of Ramjet Engine for High-Mach Integrated Control Experiment (HIMICO)-Reference-Cited by-同舟云学术

Research and Development of Ramjet Engine for High-Mach Integrated Control Experiment (HIMICO)

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Wakabayashi Sho¹,Yoshida Hidekazu¹,Chiga Takahiro¹,Sato Tetsuya¹,Taguchi Hideyuki²,Kojima Takayuki²,Okamoto Toshiki³,Ikeda Yutaka³,Nakaya Shinji³,Tsue Mitsuhiro³

Affiliation:

1. Waseda University

2. Japan Aerospace Exploration Agency (JAXA)

3. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5319

Reference9 articles.

1. Mach 4 Wind Tunnel Experiment of Hypersonic Pre-Cooled Turbojet Engine

2. [2]Tanatsugu,N.,etal.,DevelopmentStudyonATREXEngine,ActaAstronautica,Vol.41,No.12,pp.851-862,1997.

Cited by 4 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. Numerical Simulation of the Ram Combustor for High-Mach Integrated Control Experiment (HIMICO);TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021

2. Program of High Mach Integrated Control Experiment, “HIMICO” Using S-520 Sounding Rocket;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021

3. Numerical Study on the Intake Performance with Side Clearance for the High Mach Integrated Control Experiment (HIMICO);TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021

4. Integrated Design of Trajectory and Robust Control for Hypersonic Experimental Aircraft;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10