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On-line Access: 2024-08-27
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Mixing and combustion in supersonic/hypersonic flows
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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.
@article{title="Mixing and combustion in supersonic/hypersonic flows",
author="Wei Huang, Jun-tao Chang, Li Yan",
journal="Journal of Zhejiang University Science A",
volume="21",
number="8",
pages="609-613",
year="2020",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A20MCSF1"
}
%0 Journal Article
%T Mixing and combustion in supersonic/hypersonic flows
%A Wei Huang
%A Jun-tao Chang
%A Li Yan
%J Journal of Zhejiang University SCIENCE A
%V 21
%N 8
%P 609-613
%@ 1673-565X
%D 2020
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A20MCSF1
TY - JOUR
T1 - Mixing and combustion in supersonic/hypersonic flows
A1 - Wei Huang
A1 - Jun-tao Chang
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J0 - Journal of Zhejiang University Science A
VL - 21
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%@ 1673-565X
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DOI - 10.1631/jzus.A20MCSF1
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.
[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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