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
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
FLAME SPEED OF TURBULENT PREMIXED KERNEL IN TURBULENT FLOWS
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
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
TOWARDS A SIMULATION METHOD FOR ALUMINUM-PARTICLE-ENHANCED SOLID FUEL COMBUSTION DEVICES
LASER INDUCED SPARK IGNITION OF LAMINAR PREMIXED METHANE AIR JETS
FUEL SPRAY EFFECTS ON SELF-EXCITED COMBUSTION INSTABILITY IN A BLUFFBODY STABILIZED FLAME
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
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
COMBUSTOR DEVELOPMENT AND PERFORMANCE ANALYSIS FOR RECUPERATED MICROTURBINE APPLICATION
UNCERTAINTY QUANTIFICATION ANALYSIS OF RANS OF SPRAY JETS
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
MEASUREMENTS OF THE VAPOR PRESSURE OF LIQUID HYDRAZINE ABOVE ITS NORMAL BOILING POINT
NUMERICAL STUDY OF NONLINEAR SELF-SUSTAINED THERMOACOUSTIC INSTABILITY IN A SWIRLING COMBUSTOR
TURBULENT NONPREMIXED JET FLAMES UNDER TRANSVERSE ACOUSTIC FORCING