Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle
文献类型:期刊论文
作者 | Wang Y(王粤)1,2; Wang YP(汪运鹏)1,2; Jiang ZL(姜宗林)1,2 |
刊名 | PHYSICS OF FLUIDS |
出版日期 | 2023-05-25 |
卷号 | 35期号:5页码:056120 |
关键词 | Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
DOI | 10.1063/5.0151663 |
英文摘要 | Due to the complex aerodynamic interaction, the safe separation of two stages is one of the challenges for the successful launch of a two-stage-to-orbit (TSTO) vehicle. The unsteady hypersonic flow past the parallel-staged TSTO model during stage separation at Ma = 6.7 and Re = 8.86 × 105 m−1 is numerically studied using laminar flow simulation. The TSTO model consisted of a waverider and a spaceplane as booster and orbiter, respectively. The effect of the center of gravity (CoG) of the orbiter on the unsteady aerodynamic interference during stage separation of TSTO is analyzed in detail with 0.65 ≤ lCoG/lo ≤ 0.80. In addition, the aerodynamic characteristics, dynamic behaviors, and unsteady wall pressure variation are compared in different cases. The results show that the CoG regime is limited to 5% of the orbiter length for absolutely safe separation, i.e., 0.70 < lCoG/lo < 0.75. As for the unsuccessful separation, the orbiter tends to fly nose-down if lCoG/lo ≤ 0.70 while tending to pitch or somersault when lCoG/lo = 0.80. Furthermore, the pitching moment of the orbiter, which is influenced by the interstage shock wave–boundary layer interaction and shock–shock interaction, dominates the separation safety, and the specific flow mechanisms concerning the separation behavior associated with aerodynamic interference in different cases are analyzed in detail. |
学科主题 | 流体力学 ; 空气动力学 ; 计算流体力学 ; 应用力学 ; 航空、航天科学技术基础学科 ; 飞行器发射、飞行技术 |
分类号 | 一类/力学重要期刊 |
语种 | 英语 |
其他责任者 | 汪运鹏 |
源URL | [http://dspace.imech.ac.cn/handle/311007/92003] |
专题 | 力学研究所_高温气体动力学国家重点实验室 |
通讯作者 | Wang YP(汪运鹏) |
作者单位 | 1.School of Engineering Sciences, University of Chinese Academy of Sciences, 100049 Beijing, China 2.State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, 100190 Beijing, China |
推荐引用方式 GB/T 7714 | Wang Y,Wang YP,Jiang ZL. Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle[J]. PHYSICS OF FLUIDS,2023,35(5):056120. |
APA | Wang Y,Wang YP,&Jiang ZL.(2023).Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle.PHYSICS OF FLUIDS,35(5),056120. |
MLA | Wang Y,et al."Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle".PHYSICS OF FLUIDS 35.5(2023):056120. |
入库方式: OAI收割
来源:力学研究所
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