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Combustion
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Combustion Chambers
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Analysis of pressure dynamics, forced excitation and damping in a high pressure LOX/H2 combustor
Analysis of pressure dynamics, forced excitation and damping in a high pressure LOX/H2 combustor
Numerical investigation of a generic supersonic combustion chamber under realistic flight conditions
Single droplet evaporation characteristics and behaviors at higher ambient temperatures
Evaluation of the technical potential of aero engines with pressure gain combustion
Acoustic performance of bias flow liners in gas turbine combustors
Aerothermal analysis of an aeroengine annular combustor concept with angular air supply
Thermodynamic analysis and numerical modeling of supercritical injection
Thermodynamic analysis and numerical modeling of supercritical injection
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers
Investigation on heat transfer in small hydrocarbon rocket combustion chambers
Effects of combustor exit flow on turbine performance and endwall heat transfer
NOx-formation in reacting premixed jets in hot cross flow
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames