Experimental investigation and numerical simulation of secondary combustor flow in boron-based propellant ducted rocket

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机构：
[1] Hu, Jianxin
[2] Xia, Zhixun
[3] Wang, Dequan
[4] Huang, Liya
来源：
| 1600年 / Japan Society for Aeronautical and Space Sciences卷 / 56期
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Boron;
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Journal article (JA)
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