TAMARU Takashi | Aeroengine Division, National Aerospace Laboratory
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概要
Aeroengine Division, National Aerospace Laboratory | 論文
- IGTC-52 High Combustion Efficiency and NO_x Reduction by 2-Stage Combustion in Methane-Fueled Ram Combustor(Session B-8 COMBUSTION III)
- Numerical Simulation of the Hydrogen Flame Injected from Bluff-Body Type Flameholder