Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study. [PDF]
Mir A +7 more
europepmc +1 more source
Effect of Equivalence Ratio on Combustion Characteristics under Propane-Air Flame Acceleration Conditions. [PDF]
Yu Y +9 more
europepmc +1 more source
Influence of injection angles on flow structures and mixing properties in a supersonic combustor at low Mach supersonic crossflow. [PDF]
Zhang L +4 more
europepmc +1 more source
Cluster Anions of Hydrated Polycyclic Aromatic Hydrocarbons: "Magic" Water Tetramer. [PDF]
Ďurana J +5 more
europepmc +1 more source
A High-Performance Ultraviolet Optical Sensing System for Rotating Detonation Extreme Combustion. [PDF]
Dai W +7 more
europepmc +1 more source
Initiation Characteristics of Rotating Supersonic Combustion Engine
A rotating supersonic combustion engine (RSCE) is tested with various initiator tube positions along the combustion chamber to determine its impact on the ignition process. The type of fuel used is methane with oxygen as the oxidizer.
Aminuddin Saat +5 more
core
Probing Cold Supersonic Jets with Optical Frequency Combs. [PDF]
Dubroeucq R +5 more
europepmc +1 more source
Numerical investigation of low-frequency shock train oscillations in a divergent isolator with vortex generator jets. [PDF]
Wang J, He K, Zhou Q, Wang J.
europepmc +1 more source
Fuel Effects on Aviation Engine Emissions: A Chemical Reactor Network Modeling Study. [PDF]
Lopez-Pintor D +6 more
europepmc +1 more source
Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor. [PDF]
Peng SS +5 more
europepmc +1 more source

