Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles-Reference-Cited by-同舟云学术

Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Nozzles

Published:2019-01 Issue:1 Volume:35 Page:213-223
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Goto Keisuke,Nishimura Junpei,Kawasaki Akira,Matsuoka Ken,Kasahara Jiro,Matsuo Akiko¹,Funaki Ikkoh²,Nakata Daisuke,Uchiumi Masaharu,Higashino Kazuyuki

Affiliation:

1. Keio University, Yokohama 223-8522, Japan

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

Funder

The New Energy and Industrial Technology Development Organization

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

JSPS

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.B37196

Reference34 articles.

1. Review of Propulsion Applications of Detonation Waves

2. Recent Developments in the Research on Pulse Detonation Engines

3. Detonative propulsion

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

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