Aeronautical and Space Sciences Japan
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
 
Operation Characteristics of a Disktype Rotating Detonation Engine Using Hydrogen-Air Mixtures
Kazuhiro ISHII
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Keywords: Detonation, Rotating Detonation Engine, Shock Wave, Pressure Gain
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2023 Volume 71 Issue 4 Pages 99-103

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[in Japanese]
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© 2023 The Japan Society for Aeronautical and Space Sciences
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