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Characteristics and Mixing-Controlled Mechanism of Rotating Detonation Wave Under High Mach Flight Conditions

https://doi.org/10.2139/ssrn.5369724
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Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine
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Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model
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Effect of inlet and outlet boundary conditions on rotating detonation combustion
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Performance analysis of a rotating detonation combustor based on stagnation pressure measurements
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Combustion mode and wave multiplicity in rotating detonative combustion with separate reactant injection
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Investigation of pressure gain characteristics for kerosene-hot air RDE
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Theoretical analysis on the total pressure gain of rotating detonation systems
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Effects of the inflow total temperature on the non-premixed rotating detonation engine performances
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Effects of annular channel widths on wave system structures in wall-detached rotating detonation
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Experimental investigation on detonation combustion patterns of hydrogen/vitiated air within annular combustor
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Origin and chaotic propagation of multiple rotating detonation waves in hydrogen/air mixtures
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Large eddy simulation of non-reacting flow and mixing fields in a rotating detonation engine
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Experimental investigation on spray and detonation initiation characteristics of premixed/non-premixed RDE
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Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen
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Numerical investigation of wavelet features in rotating detonations with a two-step induction-reaction model
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A numerical investigation of oblique detonation waves in hydrogen-air mixtures at low mach numbers
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Research on H2/Air rotating detonation in the hollow chamber with double injection
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Effects of injection parameters on propagation patterns of hydrogen-fueled rotating detonation waves
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Numerical simulation on the operating characteristics of rotating detonation ramjet engines at high flight mach number
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Numerical investigation of the physics of rotating-detonation-engines
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Combined effect of spatial and temporal variations of equivalence ratio on combustion instability in a low-swirl combustor
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On the existence and multiplicity of rotating detonations
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Visualization and thrust measurement of rotating detonation engine with various channel expansion angles
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Analysis of flow-field characteristics and pressure gain in air-breathing rotating detonation combustor
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Characteristics of ethylene–air continuous rotating detonation in the cavity-based annular combustor
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Effects of fuel/air mixing distances on combustion instabilities in non-premixed combustion
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Propagation and heat release characteristics of rotating detonation in a ramjet engine with a divergent combustor
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Wind Tunnel Testing of a Detonation Ramjet Model at Approach Air Stream Mach Number 5.7 and a Stagnation Temperature of 1500 K
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