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.
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References
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. https://doi.org/10.1631/jzus.A1900648
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. https://doi.org/10.1631/jzus.A2000020
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. https://doi.org/10.1631/jzus.A2000042
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. https://doi.org/10.1016/j.paerosci.2018.06.003
Huang W, Du ZB, Yan L, et al., 2019. Supersonic mixing in airbreathing propulsion systems for hypersonic flights. Progress in Aerospace Sciences, 109:100545. https://doi.org/10.1016/j.paerosci.2019.05.005
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. https://doi.org/10.1631/jzus.A2000025
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. https://doi.org/10.1631/jzus.A1900349
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. https://doi.org/10.1631/jzus.A1900383
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. https://doi.org/10.1631/jzus.A2000006
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. https://doi.org/10.1631/jzus.A1900514
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. https://doi.org/10.1631/jzus.A1900565
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. https://doi.org/10.1631/jzus.A1900419
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. https://doi.org/10.1631/jzus.A1900668
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. https://doi.org/10.1631/jzus.A1900507
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. https://doi.org/10.1631/jzus.A1900392
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 (AppliedPhysics & Engineering), 21(8):684–694. https://doi.org/10.1631/jzus.A1900624
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Authors and Affiliations
Contributions
Wei HUANG wrote the manuscript. Jun-tao CHANG and Li YAN provided suggestions.
Corresponding authors
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Conflict of interest
Wei HUANG, Jun-tao CHANG, and Li YAN declare that they have no conflict of interest.
Introducing Guest Editor-in-Chief and Guest Editors:
Guest Editor-in-Chief
Dr. Wei HUANG has been the Editorial Board Member of the Journal of Zhejiang University-SCIENCE A (AppliedPhysics & Engineering) since 2018. He has been the Editorial Board Member of the Chinese Journal of Aeronautics and Aero Weaponry since 2019.
Dr. Wei HUANG is an Associate Professor at the National University of Defense Technology, China, and has been a member of the American Society of Mechanical Engineers since 2011. He was the recipient of the 2013 National Doctoral Dissertation Award, and one of the recipients of two first-class prizes in Natural Science of Hunan Province and two second-class Military Progress Prizes in Science and Technology, China. He is also an active expert on aerospace engineering in China, and in 2018 and 2019 was awarded first place among the Most Cited Chinese Researchers for his exceptional research performance in the field of aerospace engineering.
Dr. HUANG received his BS and PhD degrees from the National University of Defense Technology in 2005 and 2010, respectively. He is a researcher with over 35 invention patents, four (co)authored academic books, and over 140 technical papers published in international journals and conference proceedings. He is active in major international conferences related to aerospace engineering, and a regular reviewer for over 30 international journals. His research interests are in integrated design of hypersonic vehicles, multidisciplinary design optimization, supersonic mixing and combustion, flow control techniques, intelligent control, and hypersonic aerodynamics and thermodynamics. His findings have been successfully applied to the development of a low cost hypersonic vehicle testbed for fundamental research in China.
Guest Editors
Dr. Jun-tao CHANG is a Professor of Power Mechanism and Engineering (since 2015) at the Harbin Institute of Technology, China. He received his BS degree in 2002 and his PhD degree in 2008 in Power Mechanism and Engineering from the same Institute. He won the National Natural Science Excellent Youth Fund and the third XINGZHOU Award in 2017, the Wu Zhonghua Outstanding Young Scholar Award, and was among the Most Cited Chinese Researchers for his exceptional research performance in aerospace engineering in 2019. His current research interests focus on instability mechanisms and control of scramjets, airbreathing engine control, and the interaction mechanism between flow and combustion in scramjets. He has published over 130 peer-reviewed articles.
Dr. Li YAN is an Associate Professor of Science and Technology on Scramjet Laboratory, National University of Defense Technology, China, from where she received her PhD degree in 2006. She is a recipient of one first-class prize in Natural Science of Hunan Province and two second-class Military Progress Prizes in Science and Technology, China. Dr. YAN is a researcher with three coauthored academic books, and over 70 technical papers published in international journals and conference proceedings. Her current research interests focus on the overall design and optimization of aircraft, and the theory and application of multidisciplinary design optimization.