Cylindrical Rotating Detonation Engine with Propellant Injection Cooling-Reference-Cited by-同舟云学术

Cylindrical Rotating Detonation Engine with Propellant Injection Cooling

Published:2021-11-15 Issue: Volume: Page:1-11
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Goto Keisuke¹,Ota Kosei¹,Kawasaki Akira¹,Itouyama Noboru¹,Watanabe Hiroaki¹,Matsuoka Ken¹,Kasahara Jiro¹^ORCID,Matsuo Akiko²,Funaki Ikkoh³,Kawashima Hideto⁴

Affiliation:

1. Nagoya University, Nagoya 464-8603, Japan

2. Keio University, Yokohama 223-8522, Japan

3. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan

4. Japan Aerospace Exploration Agency, Tsukuba-Shi 305-8505, Japan

Funder

the Japan Society for the Promotion of Science

the New Energy and Industrial Technology Development Organization

the Institute of Space and Astronautical Science, the Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38427

Reference30 articles.

1. Detonative propulsion

2. Review of Propulsion Applications of Detonation Waves

3. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts

4. Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine

5. Experimental Characterization of High-Frequency Heat Flux in a Rotating Detonation Engine

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