Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
IMPROVED CHEMICAL KINETIC MODEL REDUCTION IN PYMARS FOR LIQUID PROPELLANTS
MEASUREMENT OF RAYLEIGH-BRILLOUIN SPECTRAL LINESHAPES OF COMBUSTION-RELEVANT GASES AT HIGH PRESSURE
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
FLAME SPEED OF TURBULENT PREMIXED KERNEL IN TURBULENT FLOWS
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7- ELEMENT LEAN DIRECT INJECTOR