المؤلفون: 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)

المساهمون: 林鑫

مصطلحات موضوعية: Hybrid rocket engine, Swirl injection, Novel composite fuel grain, Regression rate, Oxidizer-to-fuel ratio, REGRESSION RATE CHARACTERISTICS, PERFORMANCE, MOTOR, FLOW, Engineering, Aerospace, 二类/Q1

Relation: ACTA ASTRONAUTICA; http://dspace.imech.ac.cn/handle/311007/90343; http://dspace.imech.ac.cn/handle/311007/90344

الاتاحة: http://dspace.imech.ac.cn/handle/311007/90343
http://dspace.imech.ac.cn/handle/311007/90344
https://doi.org/10.1016/j.actaastro.2022.07.027

المؤلفون: Lin X(林鑫), Qu DD(屈丹丹), Chen XD(陈雪冬), Wang ZZ(王泽众), Luo JX(罗家枭), Meng DD(孟东东), Liu GL(刘国亮), Zhang K(张坤), Li F(李飞), Yu XL(余西龙)

المساهمون: Qu, DD, Wang, ZZ

مصطلحات موضوعية: Hybrid rocket engine, additive manufacturing, metal-nested composite fuel grain, mechanical properties, combustion properties, optical emission spectroscopy, Engineering, Manufacturing, Materials Science, Multidisciplinary, 一类

Relation: VIRTUAL AND PHYSICAL PROTOTYPING; http://dspace.imech.ac.cn/handle/311007/90224

الاتاحة: http://dspace.imech.ac.cn/handle/311007/90224
https://doi.org/10.1080/17452759.2022.2035934