斜爆轰发动机：斜爆轰波在受限空间中的起爆与稳定

张子健; 温志湧

doi:10.7638/kqdlxxb-2025.0102

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

斜爆轰发动机：斜爆轰波在受限空间中的起爆与稳定

研究专栏——爆震流动机理与推进技术专栏Ⅰ | 更新时间：2026-05-28

- 斜爆轰发动机：斜爆轰波在受限空间中的起爆与稳定
- Oblique detonation engine: Initiation and stabilization of oblique detonation waves in confined spaces
- 空气动力学学报 2025年43卷第9期页码：65-91
- 作者机构：
  
  1. 北京理工大学宇航学院,北京,100081
  2. 临近空间环境特性及效应全国重点实验室,北京,100081
  3. 香港理工大学航空及民航工程学系,香港
- 作者简介：
  
  张子健*（1992—），男，广东阳江人，教授，研究方向：激波与爆轰现象、爆轰发动机流动机理与控制. E-mail：zjzhang@bit.edu.cn
- 基金信息：
  
  国家自然科学基金（12202374）
- DOI：10.7638/kqdlxxb-2025.0102
  中图分类号： V231.3;O354.5
- 纸质出版：2025
- 稿件说明：
移动端阅览
张子健, 温志湧. 斜爆轰发动机：斜爆轰波在受限空间中的起爆与稳定[J]. 空气动力学学报, 2025, 43(9): 65−91.

ZHANG Zijian, WEN Chiyung. Oblique detonation engine: Initiation and stabilization of oblique detonation waves in confined spaces[J]. 2025, 43(9): 65-91.
张子健, 温志湧. 斜爆轰发动机：斜爆轰波在受限空间中的起爆与稳定[J]. 空气动力学学报, 2025, 43(9): 65−91. DOI： 10.7638/kqdlxxb-2025.0102

ZHANG Zijian, WEN Chiyung. Oblique detonation engine: Initiation and stabilization of oblique detonation waves in confined spaces[J]. 2025, 43(9): 65-91. DOI： 10.7638/kqdlxxb-2025.0102.

摘要

斜爆轰利用激波实现超声速气流的自增压燃烧，从而高效、快速地将化学能转化为机械能。以斜爆轰为核心燃烧组织方式的发动机，具有比冲高、可用马赫数范围广、结构紧凑等优点，被视为吸气式高马赫数推进系统极具前景的解决方案。然而，这种发动机的核心难点在于实现斜爆轰波的可靠起爆和稳定维持。由于发动机燃烧室流道空间受限，斜爆轰现象表现出与传统非受限空间不同的起爆和稳定特性。例如，有限的流道长度可能无法满足斜爆轰波起爆所需的流向距离，从而导致起爆失败或燃烧不充分；此外，燃烧室壁面的侧向约束也可能导致斜爆轰波失稳并发生前传，进而影响发动机的正常工作。因此，深入研究受限空间条件下斜爆轰波的起爆与稳定特性、流动机理及相应的流动控制方法，对于推动斜爆轰技术在推进系统中的应用至关重要。本文旨在综述受限空间斜爆轰波起爆与稳定两方面的研究进展，并在此基础上，对斜爆轰发动机在这两个方面的研究进行展望。

Abstract

Oblique detonation utilizes shock waves to achieve self-pressurized combustion in supersonic flow

enabling high-efficiency and rapid conversion of chemical energy into mechanical energy. Employing oblique detonation as the core mode for combustion organization

oblique detonation engine offers advantages such as high specific impulse

wide operable Mach number range

and compact structure

making it a highly promising solution for air-breathing high-Mach-number propulsion systems. However

the key challenges of this type of engine lie in the reliable initiation and sustained stabilization of oblique detonation waves. Due to spatial confinement of flow path in the engine combustor

the oblique detonation phenomenon exhibits different initiation and stabilization characteristics from those in conventional unconfined spaces. For example

the limited flow path length may fail to meet the streamwise distance required for oblique detonation wave initiation

leading to failed initiation or insufficient combustion. Additionally

flow constraint in the transverse directions by the combustor walls may cause destabilization and upstream propagation of oblique detonation waves

violating the normal operation of engines. Therefore

in-depth research on the initiation and stabilization characteristics

flow mechanisms

and corresponding flow control methods of oblique detonation waves under space-confined conditions is of great importance to advance the applications of oblique detonation technology in propulsion systems. This paper aims to review the research progress on both the initiation and stabilization of oblique detonation waves in confined spaces

thereby providing insights for future research on oblique detonation engines regarding these two aspects.

关键词

Keywords

references

YE Y D. Advances and prospects in hypersonic aerodynamics[J]. Chinese Science Bulletin, 2015, 60(12): 1095−1103 (in Chinese). doi: 10.1360/N972014-01180

HEISER W, PRATT D, DALEY D, et al. Hypersonic airbreathing propulsion[M]. Washington, DC: American Institute of Aeronautics and Astronautics, Inc. , 1994.

MURTHY S N B, CURRAN E T. Scramjet propulsion[M]. Reston, VA: American Institute of Aeronautics and Astronautics, 2001.

LI X Y, ZHENG X, XUE R. Current development and suggestions on scramjet propulsion technology[J]. Science and Technology China, 2019(2): 5−8 (in Chinese). doi: 10.3969/j.issn.1673-5129.2019.02.003

YUE L J, ZHANG X, ZHANG Q F, et al. Research progress on high-Mach-number scramjet engine technologies[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(2): 263−288 (in Chinese). doi: 10.6052/0459-1879-21-547

URZAY J. Supersonic combustion in air-breathing propulsion systems for hypersonic flight[J]. Annual Review of Fluid Mechanics, 2018, 50(1): 593−627. doi: 10.1146/annurev-fluid-122316-045217

JIANG Z L. Reasoning on development of air-breathing hypersonic propulsion technology[J]. Advances in Mechanics, 2009, 39(4): 398−405 (in Chinese). doi: 10.6052/1000-0992-2009-4-J2009-049

LEE J H S. The detonation phenomenon[M]. Cambridge: Cambridge University Press, 2008.

KINDRACKI J. Badania eksperymentalne i symulacje numeryczne procesu inicjacji wirującej detonacji gazowej[D]. Warszawa: Politechnika Warszawska, 2008: 167 (in Polish).

WOLANSKI P. Detonative propulsion[J]. Proceedings of the Combustion Institute, 2013, 34(1): 125−158. doi: 10.1016/j.proci.2012.10.005

WANG B, XIE Q F, WEN H C, et al. Research progress of detonation engines[J]. Journal of Propulsion Technology, 2021, 42(4): 721−737 (in Chinese). doi: 10.13675/j.cnki.tjjs.210109

LING W H, ZHOU L, TU S J, et al. Research progress and technical challenges of oblique detonation engines[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(4): 1−10 (in Chinese). doi: 10.16356/j.1005-2615.2023.04.001

ALEXANDER D C, SISLIAN J P, PARENT B. Hypervelocity Fuel/Air Mixing in Mixed-Compression Inlets of Shcramjets[J]. AIAA Journal, 2006, 44(10): 2145−2155. doi: 10.2514/1.12630

ZHANG Z J. Oblique detonation propulsion theory, technology and its experimental demonstration[D]. Beijing: Chinese Academy of Sciences, 2020 (in Chinese).

DUNLAP R A, BREHM R L, NICHOLLS J A. A preliminary study of the application of steady-state detonative combustion to a reaction engine[J]. Journal of Jet Propulsion, 1958, 28(7): 451−456. doi: 10.2514/8.7347

Teng H H, Jiang Z L. Progress in multi-wave structure and stability of oblique detonations[J]. Advances in Mechanics, 2020, 50: 202002 (in Chinese). doi: 10.16356/j.1005-2615.2023.04.001

Teng H H, Yang P F, Zhang Y N, et al. Flow and combustion mechanism of oblique detonation engines[J]. Scientia Sinica Physica, Mechanica Astronomica, 2020, 50: 090008 (in Chinese). doi: 10.1360/SSPMA-2020-0144

LI C, KAILASANATH K, ORAN E S. Detonation structures behind oblique shocks[J]. Physics of Fluids, 1994, 6(4): 1600−1611. doi: 10.1063/1.868273

VIGUIER C, SILVA L F F D, DESBORDES D, et al. Onset of oblique detonation waves: comparison between experimental and numerical results for hydrogen-air mixtures[J]. Symposium (International) on Combustion, 1996, 26(2): 3023−3031. doi: 10.1016/S0082-0784(96)80146-9

SILVA L F F D, DESHAIES B. Stabilization of an oblique detonation wave by a wedge: a parametric numerical study[J]. Combustion and Flame, 2000, 121(1-2): 152−166. doi: 10.1016/S0010-2180(99)00141-8

TENG H H, JIANG Z L. On the transition pattern of the oblique detonation structure[J]. Journal of Fluid Mechanics, 2012, 713: 659−669. doi: 10.1017/jfm.2012.478

ZHANG Y N, YANG P F, TENG H H, et al. Transition between different initiation structures of wedge-induced oblique detonations[J]. AIAA Journal, 2018, 56(10): 4016−4023. doi: 10.2514/1.J056831

YANG P F, TENG H H, JIANG Z L, et al. Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model[J]. Combustion and Flame, 2018, 193: 246−256. doi: 10.1016/j.combustflame.2018.03.026

TENG H H, TIAN C, ZHANG Y N, et al. Morphology of oblique detonation waves in a stoichiometric hydrogen–air mixture[J]. Journal of Fluid Mechanics, 2021, 913: A1. doi: 10.1017/jfm.2020.1131

LIU Y, WANG L, XIAO B G, et al. Hysteresis phenomenon of the oblique detonation wave[J]. Combustion and Flame, 2018, 192: 170−179. doi: 10.1016/j.combustflame.2018.02.010

SUN J, YANG P F, TIAN B L, et al. Effects of wedge-angle change on the evolution of oblique detonation wave structure[J]. Physics of Fluids, 2022, 34(9): 096112. doi: 10.1063/5.0102842

WANG T, ZHANG Y N, TENG H H, et al. Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture[J]. Physics of Fluids, 2015, 27(9): 096101. doi: 10.1063/1.4930986

TIAN C, TENG H H, NG H D. Numerical investigation of oblique detonation structure in hydrogen-oxygen mixtures with Ar dilution[J]. Fuel, 2019, 252(9): 496−503. doi: 10.1016/j.fuel.2019.04.126

TENG H H, NG H D, JIANG Z L. Initiation characteristics of wedge-induced oblique detonation waves in a stoichiometric hydrogen-air mixture[C]//Proceedings of the Combustion Institute. Amsterdam: Elsevier Inc, 2017, 36(2): 2735-2742. doi: 10.1016/j.proci.2016.09.025

FANG Y S, ZHANG Z J, HU Z M, et al. Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures[J]. Aerospace Science and Technology, 2019, 92(9): 676−684. doi: 10.1016/j.ast.2019.06.031

DESAI S, TAO Y J, SIVARAMAKRISHNAN R, et al. Effects of non-thermal termolecular reactions on wedge-induced oblique detonation waves[J]. Combustion and Flame, 2023, 257(3): 112−120. doi: 10.1016/j.combustflame.2023.113000

MIAO S K, ZHOU J, LIU S J, et al. Formation mechanisms and characteristics of transition patterns in oblique detonations[J]. Acta Astronautica, 2018, 142: 121−129. doi: 10.1016/j.actaastro.2017.10.035

SHI X X, XIE H P, ZHOU L, et al. A theoretical criterion on the initiation type of oblique detonation waves[J]. Acta Astronautica, 2022, 190: 342−348. doi: 10.1016/j.actaastro.2021.10.005

RUEGG F W, DORSEY W W. A missile technique for the study of detonation waves[J]. Journal of Research of the National Bureau of Standards – C. Engineering and Instrumentation, 1962, 66C(1): 51–58. doi: 10.6028/jres.066C.007

LEHR H F. Experiments on shock-induced combustion[J]. Astronautica Acta, 1972, 17(4-5): 589−597.

HIGGINS A, BRUCKNER A. Experimental investigation of detonation initiation by hypervelocity blunt projectiles[C]//34th Aerospace Sciences Meeting and Exhibit. Reno, NV: American Institute of Aeronautics and Astronautics, 1996. doi: 10.2514/6.1996-342

VASILJEV A A. Initiation of gaseous detonation by a high speed body[J]. Shock Waves, 1994, 3(4): 321−326. doi: 10.1007/BF01415830

JU Y G, MASUYA G, SASOH A. Numerical and theoretical studies on detonation initiation by a supersonic projectile[J]. Symposium (International) on Combustion, 1998, 27(2): 2225−2231. doi: 10.1016/S0082-0784(98)80071-4

VERREAULT J, HIGGINS A J. Initiation of detonation by conical projectiles[J]. Proceedings of the Combustion Institute, 2011, 33(2): 2311−2318. doi: 10.1016/j.proci.2010.07.086

XIANG G X, LI X D, SUN X F, et al. Investigations on oblique detonations induced by a finite wedge in high altitude[J]. Aerospace Science and Technology, 2019, 95: 105451. doi: 10.1016/j.ast.2019.105451

FANG Y S, HU Z M, TENG H H. Numerical investigation of oblique detonations induced by a finite wedge in a stoichiometric hydrogen-air mixture[J]. Fuel, 2018, 234: 502−507. doi: 10.1016/j.fuel.2018.07.048

ZHANG Y C, XIANG G X, TU Q R, et al. The initiation characteristics of oblique detonation in acetylene-air mixtures in the finite wedge[J]. Acta Mechanica Sinica, 2023, 39(3): 122231. doi: 10.1007/s10409-022-22231-x

GAO Y, LI H Y, XIANG G X, et al. Initiation characteristics of oblique detonation waves from a finite wedge under argon dilution[J]. Chinese Journal of Aeronautics, 2021, 34(10): 81−90. doi: 10.1016/j.cja.2020.11.013

LIU Y, HAN X D, YAO S B, et al. A numerical investigation of the prompt oblique detonation wave sustained by a finite-length wedge[J]. Shock Waves, 2016, 26(6): 729−739. doi: 10.1007/s00193-016-0626-3

QIN J X, ZHU D H. Criticality for oblique detonation waves induced by a finite wedge in a hydrogen–air mixture[J]. Aerospace, 2023, 10(6): 508. doi: 10.3390/aerospace10060508

TENG H H, LIU S Y, LI Z Z, et al. Effect of ozone addition on oblique detonations in hydrogen-air mixtures[J]. Applied Thermal Engineering, 2024, 240: 122292. doi: 10.1016/j.applthermaleng.2023.122292

VASHISHTHA A, PANIGRAHY S, CAMPI D, et al. Oblique detonation wave control with O3 and H2O2 sensitization in hypersonic flow[J]. Energies, 2022, 15(11): 4140. doi: 10.3390/en15114140

ZHANG Y C, XIANG G X. Investigations on the initiation characteristics of radical-assisted oblique detonation waves generated by plasma discharges[J]. Aerospace Science and Technology, 2024, 153: 109466. doi: 10.1016/j.ast.2024.109466

XI X C, TIAN C, WANG K L. Effects of hydrogen addition on oblique detonations in methane–air mixtures[J]. International Journal of Hydrogen Energy, 2022, 47(13): 8621−8629. doi: 10.1016/j.ijhydene.2021.12.195

GONG J S, ZHANG Y N, PAN H, et al. Experimental investigation on initiation of oblique detonation waves[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, China: American Institute of Aeronautics and Astronautics, 2017. doi: 10.2514/6.2017-2350

QIN Q Y, ZHANG X B. A novel method for trigger location control of the oblique detonation wave by a modified wedge[J]. Combustion and Flame, 2018, 197: 65−77. doi: 10.1016/j.combustflame.2018.07.011

HAN X, ZHANG W S, ZHANG Z J, et al. Numerical study on oblique detonation waves induced by a bump[J]. Journal of Propulsion Technology, 2022, 43(5): 185−196 (in Chinese). doi: 10.13675/j.cnki.tjjs.200853

XIANG G X, ZHANG Y C, ZHANG C F, et al. Study on initiation mechanism of oblique detonation induced by blunt bump on wedge surface[J]. Fuel, 2022, 323: 124314. doi: 10.1016/j.fuel.2022.124314

ZHANG Y C, XIANG G X, YU J, et al. Accelerated initiation of oblique detonation induced by disturbance in detonative zone[J]. Chinese Journal of Aeronautics, 2023, 36(11): 153−164. doi: 10.1016/j.cja.2023.09.031

HAN X, LIU Y F, ZHANG Z J, et al. Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model[J]. Combustion and Flame, 2023, 258: 113102. doi: 10.1016/j.combustflame.2023.113102

TENG H H, ZHANG Y H, YANG P F, et al. Oblique detonation wave triggered by a double wedge in hypersonic flow[J]. Chinese Journal of Aeronautics, 2022, 35(4): 176−184. doi: 10.1016/j.cja.2021.07.040

XIONG H C, QIU R F, HAN X, et al. Investigating the flow characteristics and thermodynamic performance of curved detonation waves[J]. Physics of Fluids, 2023, 35(8): 087119. doi: 10.1063/5.0157789

ZHANG Z J, JIANG Z Q. Numerical investigation of transverse-jet-assisted initiation of oblique detonation waves in a combustor[J]. Aerospace, 2023, 10(12): 1033. doi: 10.3390/aerospace10121033

ZHANG Y C, XIANG G X, GAO X, et al. Study on initiation characteristics of oblique detonation induced by hydrogen jets in acetylene-air mixtures[J]. Fuel, 2023, 350: 128787. doi: 10.1016/j.fuel.2023.128787

FAN J, ZHANG Y C, XIANG G X, et al. Numerical investigation of sweeping jet actuator on oblique detonation[J]. Combustion and Flame, 2024, 268: 113622. doi: 10.1016/j.combustflame.2024.113622

YAO J Y, LIN Z Y. Numerical investigation of jet-wedge combinatorial initiation for oblique detonation wave in supersonic premixed mixture[J]. Physics of Fluids, 2023, 35(2): 026101. doi: 10.1063/5.0136455

HAN X, QIU R F, YOU Y C. Flow characteristics and propulsive performance of oblique detonation waves induced by a transverse jet[J]. Physics of Fluids, 2024, 36: 076133. doi: 10.1063/5.0216594

BAO Y, QIU R F, LOU J H, et al. Deep learning-based prediction of initiation jet momentum ratio in jet-induced oblique detonations[J]. Aerospace Science and Technology, 2024, 155: 109724. doi: 10.1016/j.ast.2024.109724

ZHANG W S, ZHANG Z J, JIANG Z L, et al. Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition[J]. AIP Advances, 2021, 11(12): 125119. doi: 10.1063/5.0073035

JIANG Z Q, CHEN Z N, SHI L S, et al. Numerical study of oblique detonation initiation assisted by local energy deposition[OL]. arXiv: 2508.08943 [physics. flu-dyn], 2025. doi: 10.48550/arXiv.2508.08943

ZHANG Z J, WEN C Y, YUAN C K, et al. An experimental study of formation of stabilized oblique detonation waves in a combustor[J]. Combustion and Flame, 2022, 237: 111868. doi: 10.1016/j.combustflame.2021.111868

CATHEY C, WANG F, TANG T, et al. Transient plasma ignition for delay reduction in pulse detonation engines[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: American Institute of Aeronautics and Astronautics, 2007. doi: 10.2514/6.2007-443

ISHIHARA S, SUZUKI K, INOUE H, et al. Critical energy for direct initiation of detonation induced by laser ablation[J]. Shock Waves, 2016, 26(5): 635−643. doi: 10.1007/s00193-015-0617-9

STARIKOVSKIY A, ALEKSANDROV N. Plasma-assisted ignition and combustion[J]. Progress in Energy and Combustion Science, 2013, 39(1): 61−110. doi: 10.1016/j.pecs.2012.05.003

JU Y G, SUN W T. Plasma assisted combustion: Dynamics and chemistry[J]. Progress in Energy and Combustion Science, 2015, 48(6): 21−83. doi: 10.1016/j.pecs.2014.12.002

CARRIER G, FENDELL F, MCGREGOR R, et al. Laser-initiated conical detonation wave for supersonic combustion[J]. Journal of Propulsion and Power, 1992, 8(2): 472−480. doi: 10.2514/3.23501

FENDELL F, MITCHELL J, MCGREGOR R, et al. Laser-initiated conical detonation wave for supersonic combustion. II[J]. Journal of Propulsion and Power, 1993, 9(2): 182−190. doi: 10.2514/3.23607

MASUYA G, TAKITA K, TAKAHASHI K, et al. Effects of airstream Mach number on H/N plasma igniter[J]. Journal of Propulsion and Power, 2002, 18(3): 679−685. doi: 10.2514/2.5984

TAKITA K, UEMOTO T, SATO T, et al. Ignition characteristics of plasma torch for hydrogen jet in an airstream[J]. Journal of Propulsion and Power, 2000, 16(2): 227−233. doi: 10.2514/2.5587

LOVASCIO S, OMBRELLO T, HAYASHI J, et al. Effects of pulsation frequency and energy deposition on ignition using nanosecond repetitively pulsed discharges[J]. Proceedings of the Combustion Institute, 2017, 36(3): 4079−4086. doi: 10.1016/j.proci.2016.07.065

PRATT D T, HUMPHREY J W, GLENN D E. Morphology of standing oblique detonation waves[J]. Journal of Propulsion and Power, 1991, 7(5): 837−845. doi: 10.2514/3.23399

ZHANG Z J, WEN C Y, ZHANG W S, et al. A theoretical method for solving shock relations coupled with chemical equilibrium and its applications[J]. Chinese Journal of Aeronautics, 2022, 35(6): 47−62. doi: 10.1016/j.cja.2021.08.021

LI H Y, ZHANG Z J, YAO K, et al. On theoretical modeling of underdriven oblique detonation phenomenon[J]. Physics of Fluids, 2025, 37. doi: 10.1063/5.0285978

VERREAULT J, HIGGINS A J, STOWE R A. Formation and structure of steady oblique and conical detonation waves[J]. AIAA Journal, 2012, 50(8): 1766−1772. doi: 10.2514/1.J051632

KASAHARA J, ARAI T, MATSUO A, et al. Experimental investigations of steady-state oblique detonation waves generated around hypersonic projectiles[C]//10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference. Kyoto, Japan: American Institute of Aeronautics and Astronautics, 2001. doi: 10.2514/6.2001-1800

MAEDA S, SUMIYA S, KASAHARA J, et al. Initiation and sustaining mechanisms of stabilized oblique detonation waves around projectiles[J]. Proceedings of the Combustion Institute, 2013, 34(2): 1973−1980. doi: 10.1016/j.proci.2012.05.035

WEN C Y, HORNUNG H G. Non-equilibrium dissociating flow over spheres[J]. Journal of Fluid Mechanics, 1995, 299: 389−405. doi: 10.1017/S0022112095003545

OLIVIER H. A theoretical model for the shock stand-off distance in frozen and equilibrium flows[J]. Journal of Fluid Mechanics, 2000, 413: 345−353. doi: 10.1017/S0022112000008703

MATSUO A, FUJII K. Prediction method of unsteady combustion around hypersonic projectile in stoichiometric hydrogen-air[J]. AIAA Journal, 1998, 36(10): 1834−1841. doi: 10.2514/2.299

WANG K L, YANG P F, TENG H H. Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner[J]. Aerospace Science and Technology, 2021, 112: 106592. doi: 10.1016/j.ast.2021.106592

YAN H, HAN X, XIONG H C, et al. Curved detonation and its reflections[J]. Journal of Fluid Mechanics, 2024, 984: A11. doi: 10.1017/jfm.2024.142

XIONG H C, QIU R F, ZHANG T, et al. Characteristics of hypersonic inward turning detonation wave[J]. Chinese Journal of Aeronautics, 2025, 38(4): 103330. doi: 10.1016/j.cja.2024.103330

ESS P R, SISLIAN J P, ALLEN C B. Blunt-body generated detonation in viscous hypersonic ducted flows[J]. Journal of Propulsion and Power, 2005, 21(4): 667−680. doi: 10.2514/1.5579

SUN J, YANG P F, CHEN Z. Dynamic interaction patterns of oblique detonation waves with boundary layers in hypersonic reactive flows[J]. Combustion and Flame, 2025, 271: 113832. doi: 10.1016/j.combustflame.2024.113832

XIANG G X, ZHANG Y C, GAO X, et al. Oblique detonation waves induced by two symmetrical wedges in hydrogen-air mixtures[J]. Fuel, 2021, 295: 120615. doi: 10.1016/j.fuel.2021.120615

XIANG G X, LI H Y, ZHANG G Q, et al. Characteristics of the oblique detonation flow field induced by a complex wave structure[J]. International Journal of Hydrogen Energy, 2021, 46(33): 17435−17445. doi: 10.1016/j.ijhydene.2021.02.163

LU F K, FAN H Y, WILSON D R. Detonation waves induced by a confined wedge[J]. Aerospace Science and Technology, 2006, 10(8): 679−685. doi: 10.1016/j.ast.2006.06.005

HIGGINS A J, KNOWLEN C, BRUCKNER A P. Ram accelerator operating limits, part 2: nature of observed limits[J]. Journal of Propulsion and Power, 1998, 14(6): 959−966. doi: 10.2514/2.5360

YATSUFUSA T, TAKI S. Visualization of burning flow around a ram accelerator projectile by coaxial simultaneous shadow/direct photography[J]. Shock Waves, 2002, 12(3): 235−240. doi: 10.1007/s00193-002-0154-1

WANG K L, ZHANG Z J, YANG P F, et al. Numerical study on reflection of an oblique detonation wave on an outward turning wall[J]. Physics of Fluids, 2020, 32(4): 046101. doi: 10.1063/5.0001845

ZHANG Z J, LIU Y F, WEN C Y. Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner[J]. Journal of Fluid Mechanics, 2022, 940: A29. doi: 10.1017/jfm.2022.226

ZHANG Z J, LIU Y F, JIANG Z L, et al. Study on stabilization characteristics of oblique detonation waves in combustion chambers[C]//Proc. of the 18th National Conference on Shock Waves and Shock Tubes. Beijing Fengtai: The Chinese Society of Theoretical Applied Mechanics, 2018 (in Chinese).

DELERY J M. Shock wave/turbulent boundary layer interaction and its control[J]. Progress in Aerospace Sciences, 1985, 22(4): 209−280. doi: 10.1016/0376-0421(85)90001-6

BABINSKY H, OGAWA H. SBLI control for wings and inlets[J]. Shock Waves, 2008, 18(2): 89−96. doi: 10.1007/s00193-008-0149-7

ZHANG Z J, MA K F, ZHANG W S, et al. Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection[J]. Aerospace Science and Technology, 2020, 105: 106054. doi: 10.1016/j.ast.2020.106054

ZHANG Z J, WEN C Y, ZHANG W S, et al. Formation of stabilized oblique detonation waves in a combustor[J]. Combustion and Flame, 2021, 223: 423−436. doi: 10.1016/j.combustflame.2020.09.034

ALEXANDER D C, SISLIAN J P. Computational study of the propulsive characteristics of a shcramjet engine[J]. Journal of Propulsion and Power, 2008, 24(1): 34−44. doi: 10.2514/1.29951

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

基于非线性耦合本构关系的高速磁流体控制数值模拟

开槽轨道对高速磁浮列车气动特性的影响

临近空间长航时无人机飞发一体气动设计研究进展

侧壁约束下三维燃烧室斜爆轰结构的数值研究

“无人机飞发气动综合设计”专栏序言