EVALUATION OF AIR-BLAST ATOMIZERS FOR MIXING, COMBUSTION IN SUPERSONIC FLOWS
COMBUSTION BEHAVIOR OF AMMONIUM PERCHLORATE AT HIGH PRESSURES
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)
SMALL-VOLUME, HIGH-THROUGHPUT TECHNIQUES FOR FUEL PHYSICAL PROPERTY MEASUREMENTS
TRANSVERSE COMBUSTION INSTABILITIES IN A HIGH PRESSURE MULTI-ELEMENT COMBUSTOR
INFLUENCE OF COMPRESSIBILITY EFFECT ON SUPERSONIC COMBUSTION MODELING
FUEL SENSITIVITY OF LEAN BLOWOUT IN A RQL GAS TURBINE COMBUSTOR
IGNITION OF JET FUEL ASSISTED BY A HOT SURFACE AT AIRCRAFT COMPRESSION IGNITION ENGINE CONDITIONS
HIGH-SPEED VIDEO ANALYSIS OF LUBRICATING OILS UNDERGOING HOT-SURFACE IGNITION
HIGH SPEED DIAGNOSTICS USING CHEMILUMINESCENCE THERMOMETRY IN A SHOCK TUBE
INVESTIGATION OF SPRAY CHARACTERISTICS IN SINGLE ELEMENT LEAN DIRECT INJECTION COMBUSTOR
MEASUREMENTS OF THE VAPOR PRESSURE OF LIQUID HYDRAZINE ABOVE ITS NORMAL BOILING POINT
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
COMBUSTION OF BORON, MAGNESIUM DIBORIDE PARTICLES IN LOW EQUIVALENCE RATIO METHANE FLAMES
DESIGN AND TEST OF A SHOCK TUBE FACILITY TO INVESTIGATE DROPLET AEROBREAKUP
MANUFACTURING, BURNING OF COMPOSITE AP/HTPB/AP LAMINATE PROPELLANTS
LAGRANGIAN FLAME-VORTICITY CHARACTERIZATION OF BLUFF-BODY FLAME BLOWOUT
CHARACTERISTICS OF A PREMIXED REACTING JET-IN-CROSSFLOW AT ELEVATED PRESSURES
APPLICATION OF DYNAMIC ZONE FLAMELET MODEL TO A GH2/GO2 ROCKET COMBUSTOR
VALIDATION OF A MOMENT-BASED SOOT MODEL ON BENCHMARK, PRODUCTION AIRCRAFT ENGINE COMBUSTORS