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Effects of pulse injection on the flow field structure and combustion performance in a kerosene-fueled supersonic combustor
点击次数:
所属单位:40200
发表刊物:ACTA ASTRONAUTICA
ISSN号:0094-5765
是否译文:否
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点击次数:
所属单位:40200
发表刊物:ACTA ASTRONAUTICA
ISSN号:0094-5765
是否译文:否