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
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
COMBUSTOR DEVELOPMENT AND PERFORMANCE ANALYSIS FOR RECUPERATED MICROTURBINE APPLICATION
LASER-SUPPORTED PLASMA EMISSION AND RADIATION WAVE
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)