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On-line Access: 2020-06-10

Received: 2020-07-15

Revision Accepted: 2020-07-24

Crosschecked: 2020-07-25

Cited: 0

Clicked: 206

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Wei Huang

https://orcid.org/0000-0001-9805-985X

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Journal of Zhejiang University SCIENCE A 2020 Vol.21 No.8 P.609-613

http://doi.org/10.1631/jzus.A20MCSF1


Mixing and combustion in supersonic/hypersonic flows


Author(s):  Wei Huang, Jun-tao Chang, Li Yan

Affiliation(s):  Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China; more

Corresponding email(s):   gladrain2001@163.com, changjuntao@hit.edu.cn, scarlet@163.com

Key Words:  Mixing, Combustion, Supersonic/Hypersonic flow


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Wei Huang, Jun-tao Chang, Li Yan. Mixing and combustion in supersonic/hypersonic flows[J]. Journal of Zhejiang University Science A, 2020, 21(8): 609-613.

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year="2020",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A20MCSF1"
}

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TY - JOUR
T1 - Mixing and combustion in supersonic/hypersonic flows
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Abstract: 
In this special issue, we invited primary scientists on the leading edge in this field and with recent high impact research to share their expertise and perspectives. The collected papers cover various topics, such as shock wave/turbulence boundary layer interaction control, mixing, ignition, and flame stabilization in scramjet combustors, and mode transition in rotating detonation engines.

超/高超声速气流中的混合与燃烧

概要:在国家自然科学基金两期重大研究计划的指导下,高超声速技术越来越成熟,尤其是它的核心组成部分--吸气式高超声速推进系统. 为了满足单级/两级入轨可重复使用飞行器以及高超声速飞机对动力装置的需求,非常有必要发展一些新概念组合循环发动机方案. 但是,由于高速气流在超燃冲压发动机燃烧室内的滞留时间非常有限,只有毫秒量级,所以在如此快的流速下通过加热来获取有用推力仍然极具挑战性. 为此,学者们提出了许多混合增强措施,包括超/高超声速气流中的火焰传播与稳定机制. 本专辑收集了相关科研人员在设计理论、数值仿真、地面风洞试验等方面取得的一批核心技术成果,包括激波/湍流边界层干扰控制,隔离段中激波串与湍流边界层之间的强干扰,超燃冲压发动机燃烧室中的混合、点火与火焰稳定,以及旋转爆震发动机中的模态转换等. 这些研究对大尺度发动机的工程化具有重要的参考价值.
关键词:混合; 燃烧; 超/高超声速气流; 模态转换; 激波/边界层干扰

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

Reference

[1]Chen K, Liang WC, Liu MX, et al., 2020. Comparison of geomagnetic aided navigation algorithms for hypersonic vehicles. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):673-683.

[2]Chen SH, Liu J, Huang W, et al., 2020. Design methodology of an osculating cone waverider with adjustable sweep and dihedral angles. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):770-782.

[3]Hou WX, Chang JT, Kong C, et al., 2020. Experimental study and analysis of shock train self-excited oscillation in an isolator with background waves. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):614-635.

[4]Huang W, Du ZB, Yan L, et al., 2018. Flame propagation and stabilization in dual-mode scramjet combustors: a survey. Progress in Aerospace Sciences, 101:13-30.

[5]Huang W, Du ZB, Yan L, et al., 2019. Supersonic mixing in airbreathing propulsion systems for hypersonic flights. Progress in Aerospace Sciences, 109:100545.

[6]Jiang H, Liu J, Luo SC, et al., 2020. Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):745-760.

[7]Lei ZD, Chen ZW, Yang XQ, et al., 2020a. Operational mode transition in a rotating detonation engine. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):721-733.

[8]Lei ZD, Yang XQ, Ding J, et al., 2020b. Performance of rotating detonation engine with stratified injection. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):734-744.

[9]Li L, Wang HB, Zhao GY, et al., 2020. Efficient WENOCU4 scheme with three different adaptive switches. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):695-720.

[10]Shen BX, Liu HP, Liu WQ, 2020. Influence of angle of attack on a combined opposing jet and platelet transpiration cooling blunt nose in hypersonic vehicle. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(9):761-769.

[11]Shi W, Tian Y, Zhang WZ, et al., 2020. Experimental investigation on flame stabilization of a kerosene-fueled scramjet combustor with pilot hydrogen. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):663-672.

[12]Sun YC, Cai Z, Wang TY, et al., 2020. Numerical study on cavity ignition process in a supersonic combustor. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), in press.

[13]Yan XT, Xia ZX, Huang LY, et al., 2020. Numerical and experimental study on the combustion of NEPE propellants. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), in press.

[14]Zhang BH, Zhao YX, Liu J, 2020. Effects of bleed hole size on supersonic boundary layer bleed mass flow rate. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):652-662.

[15]Zhao YH, Liang JH, Zhang SP, et al., 2020. Experimental investigation on flow characteristics of a transverse jet with an upstream vortex generator. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):636-651.

[16]Zhou R, Shen CB, Jin X, 2020. Numerical study on the morphology of a liquid-liquid pintle injector element primary breakup spray. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 21(8):684-694.

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