39th CFD Symposium
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Presentation Information

9:10 AM - 9:30 AM JST(12:10 AM - 12:30 AM UTC)

[OS3-1-1-02]Comparison of Combustion Instability Characteristics of H2/O2 and CH4/O2 in a High-Pressure Rocket Combustor

*Riku Shimoyama1, Hiroshi Terashima1 (1. Hokkaido University)

Keywords:

rocket engine,combustion instability,detailed reaction mechanisms

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