Review of combustion stabilization for hypersonic airbreathing propulsion
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
Research progress on strut-equipped supersonic combustors for scramjet application
Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …
supersonic flight conditions, and combustors are critical components in scramjet engines …
A review of aircraft subsonic and supersonic combustors
Combustion is an essential process for generating propulsion for most existing aircraft. The
combustion processes, such as ignition, flame propagation, and flame stability, are …
combustion processes, such as ignition, flame propagation, and flame stability, are …
高马赫数超燃冲压发动机技术研究进展
岳连捷， 张旭， 张启帆， 陈科挺， 李进平， 陈昊， 姚卫… - 力学学报, 2022 - lxxb.cstam.org.cn
吸气式高超声速飞行在空间运输和国家空天安全领域具有极高价值, 超燃冲压发动机是其核心
动力装置. 目前飞行马赫数4.0~ 7.0 超燃冲压发动机技术日趋成熟, 发展更高速的飞行动力技术 …
动力装置. 目前飞行马赫数4.0~ 7.0 超燃冲压发动机技术日趋成熟, 发展更高速的飞行动力技术 …
Advances and challenges in modeling high-speed turbulent combustion in propulsion systems
ED Gonzalez-Juez, AR Kerstein, R Ranjan… - Progress in Energy and …, 2017 - Elsevier
Combustion environments in propulsion systems involve the interaction of a variety of
physics. In devices such as augmentors, ramjets and scramjets, such environments include …
physics. In devices such as augmentors, ramjets and scramjets, such environments include …
Effect of parametric variation of strut layout and position on the performance of a typical two-strut based scramjet combustor
The two equation Shear stress transport k-ω turbulence model and the 2D compressible
Reynolds-Averaged Navier–Stokes (RANS) equations along with single-step chemical …
Reynolds-Averaged Navier–Stokes (RANS) equations along with single-step chemical …
Finite rate chemistry large-eddy simulation of self-ignition in supersonic combustion ramjet
M Berglund, E Fedina, C Fureby, J Tegnér… - AIAA journal, 2010 - arc.aiaa.org
In this study, large-eddy simulation is used to analyze supersonic flow, mixing, and
combustion in a supersonic combustor equipped with a two-stage fuel injector strut. The …
combustion in a supersonic combustor equipped with a two-stage fuel injector strut. The …
A computational study of supersonic combustion in strut injector and hypermixer flow fields
C Fureby, K Nordin-Bates, K Petterson… - Proceedings of the …, 2015 - Elsevier
Achieving sufficiently high combustion efficiency and stability in supersonic combustion is
extremely challenging and highly dependent on the fuel-injection and mixing strategies …
extremely challenging and highly dependent on the fuel-injection and mixing strategies …
Research on combustion stability characteristics of scramjet combustor equipped with strut injector
F Quan, J Chang, C Lv, G Wu, C Kong - Applied Thermal Engineering, 2025 - Elsevier
The combustor is the core component of the scramjet engine, and stable combustion is the
prerequisite for the efficient operation of the scramjet engine. At present, researchers premix …
prerequisite for the efficient operation of the scramjet engine. At present, researchers premix …
Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor
M Sun, Z Zhong, J Liang, H Wang - Acta astronautica, 2016 - Elsevier
Supersonic combustion with cavity-strut injection of supercritical kerosene in a model
scramjet engine was experimentally investigated in Mach 2.92 facility with the stagnation …
scramjet engine was experimentally investigated in Mach 2.92 facility with the stagnation …