Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
TOWARDS A SIMULATION METHOD FOR ALUMINUM-PARTICLE-ENHANCED SOLID FUEL COMBUSTION DEVICES
LASER INDUCED SPARK IGNITION OF LAMINAR PREMIXED METHANE AIR JETS
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
EXPERIMENTAL AND NUMERICAL STUDY OF METHANE-OXYGEN COMBUSTION INSIDE A LOW PRESSURE ROCKET MOTOR
PERFORMANCE COMPARISON OF DATA-DRIVEN REDUCED MODELS FOR A SINGLEINJECTOR COMBUSTION PROCESS
PINTLE INJECTOR SPRAY ATOMIZATION: LIQUID SHEET BREAKUP QUANTIFICATION
DEVELOPMENT AND TESTING OF PULSE GUNS FOR COMBUSTION INSTABILITY TESTING
BROADBAND, MID-INFRARED LASER-ABSORPTION MEASUREMENTS OF TEMPERATURE, CH4, AND C3H8 IN FLAMES
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7- ELEMENT LEAN DIRECT INJECTOR
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
IMPROVED CHEMICAL KINETIC MODEL REDUCTION IN PYMARS FOR LIQUID PROPELLANTS
MEASUREMENT OF RAYLEIGH-BRILLOUIN SPECTRAL LINESHAPES OF COMBUSTION-RELEVANT GASES AT HIGH PRESSURE
FUEL SPRAY EFFECTS ON SELF-EXCITED COMBUSTION INSTABILITY IN A BLUFFBODY STABILIZED FLAME
COMBUSTOR DEVELOPMENT AND PERFORMANCE ANALYSIS FOR RECUPERATED MICROTURBINE APPLICATION
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
EVALUATION OF PLATEAU BURNING BEHAVIOR IN HTPB-AP-AL COMPOSITE PROPELLANTS