Supersonic Combustion using Multiple Stinger-shaped Injectors-Reference-Cited by-同舟云学术

Supersonic Combustion using Multiple Stinger-shaped Injectors

Published:2017 Issue:1 Volume:60 Page:56-59
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

KOUCHI Toshinori¹,TOMIOKA Sadatake²,HIRANO Kohshi³,MATSUO Akiko³,MASUYA Goro⁴

Affiliation:

1. Department of Mechanical and System Engineering, Okayama University

2. Research and Development Directorate, Japan Aerospace Exploration Agency

3. Department of Mechanical Engineering, Keio University

4. Center for Education and Research on Science for Global Safety, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

Reference15 articles.

Cited by 3 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

2. Research on Fuel Mixing in a Non-reacting Situation Simulating a Dual-mode Combustor;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2019