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Creator:李飞
First author
Creator:林鑫
Funding Organization:National Key Project
Funding Project:National Natural Science Foundation of China[11872368]
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
Authors:
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Luo JX(罗家枭)
;
Fang SH(方思晗)
;
Zhang CY(张春元)
;
Li F(李飞)
;
Yu XL(余西龙)
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Submit date:2022/11/08
Hybrid rocket engine
Swirl injection
Novel composite fuel grain
Regression rate
Oxidizer-to-fuel ratio