Flame propagation and stabilization in dual-mode scramjet combustors: a survey
W Huang, Z Du, L Yan, R Moradi - Progress in Aerospace Sciences, 2018 - Elsevier
The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …
Research and development on inlets for rocket based combined cycle engines
L Shi, Y Yang, G Zhao, P Liu, D Zhao, F Qin… - Progress in Aerospace …, 2020 - Elsevier
Rocket based combined cycle (RBCC) engine is regarded as one of the most efficient
propulsion systems for reusable space transportation vehicles and hypersonic cruise …
propulsion systems for reusable space transportation vehicles and hypersonic cruise …
Experimental detection of two-dimensional temperature distribution in rocket-based combined cycle combustion chamber using multispectral imaging processing
The extremely harsh environment and highly unsteady and transient nature during
supersonic combustion bring great challenges for quantitative diagnostics. In the present …
supersonic combustion bring great challenges for quantitative diagnostics. In the present …
Behaviors of the reacting flowfield during the spontaneous formation of ramjet mode under a supersonic inflow
TY Wang, Z Cai, B An, JR Wang, MB Sun, CH Liang… - Physics of …, 2023 - pubs.aip.org
This work experimentally studied the formation process of the ramjet mode occurring in a
cavity-based combustor operating at a high-enthalpy supersonic flow. The ramjet mode is …
cavity-based combustor operating at a high-enthalpy supersonic flow. The ramjet mode is …
An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission
The rocket-based combined cycle (RBCC) engine is believed to be an ideal propulsion
system for the space round trip mission in the future. The mission planning process is limited …
system for the space round trip mission in the future. The mission planning process is limited …
Modelling n-heptane dilute spray flames in a model supersonic combustor fueled by hydrogen
Combustion characteristics of n-heptane dilute sprays in a model supersonic combustor
fueled by hydrogen are numerically investigated. The two-phase compressible reactive …
fueled by hydrogen are numerically investigated. The two-phase compressible reactive …
Combustion mode and heat release characteristics of a kerosene-fueled rocket-aided ramjet combustor in ramjet-to-scramjet mode transition
G Zhao, Z Tian, H Pan, L Shi, G He - Aerospace Science and Technology, 2023 - Elsevier
In this study, a rocket-aided ramjet engine (RARE) configuration is proposed that is aimed at
improving the thrust gap and enhancing the engine thrust stability in the ramjet-to-scramjet …
improving the thrust gap and enhancing the engine thrust stability in the ramjet-to-scramjet …
The overall layout of rocket-based combined-cycle engines: a review
T Zhang, Z Wang, W Huang, J Chen, M Sun - Journal of Zhejiang …, 2019 - Springer
Rocket-based combined-cycle (RBCC) engines are known as the most promising type of
engine with the potential to realize 'single stage to orbit'(SSTO). This will dramatically reduce …
engine with the potential to realize 'single stage to orbit'(SSTO). This will dramatically reduce …
Rocket-augmented flame stabilization and combustion in a cavity-based scramjet
L Shi, Z Tian, C Dai, W Zhang, Z Wei, G Zhao… - Aerospace Science and …, 2023 - Elsevier
The scramjet engine has become an important propulsion system in hypersonic vehicles for
its high specific impulse, but it also has obvious shortcomings, such as narrow reliable …
its high specific impulse, but it also has obvious shortcomings, such as narrow reliable …
[HTML][HTML] Numerical study on the lobed nozzles for enhancing the mixing and combustion performance of rocket-based combined cycle engine
K Wang, F Li, K Zhao, T Zhou - Energy Reports, 2022 - Elsevier
Space exploration is economically feasible with the development of aerospace technology.
The Mach number limit of the aircraft depends on the structure of aeroengine. Rocket engine …
The Mach number limit of the aircraft depends on the structure of aeroengine. Rocket engine …