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
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
MEASUREMENTS OF THE VAPOR PRESSURE OF LIQUID HYDRAZINE ABOVE ITS NORMAL BOILING POINT
COMBUSTOR DEVELOPMENT AND PERFORMANCE ANALYSIS FOR RECUPERATED MICROTURBINE APPLICATION
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
DETERMINATION OF HEAT OF VAPORIZATION AND VAPOR PRESSURE BY MICRO-LITER FUEL DROPLET VAPORIZATION
IMPROVED CHEMICAL KINETIC MODEL REDUCTION IN PYMARS FOR LIQUID PROPELLANTS
MEASUREMENT OF RAYLEIGH-BRILLOUIN SPECTRAL LINESHAPES OF COMBUSTION-RELEVANT GASES AT HIGH PRESSURE
BURNING RATE CHARACTERIZATION OF AMMONIUM PERCHLORATE PELLETS CONTAINING CATALYTIC ADDITIVES
STUDY OF COMBUSTION INSTABILITIES IN TRANSVERSE INSTABILITY CHAMBER USING FLAME TRANSFER FUNCTIONS
LARGE-EDDY SIMULATION OF SPRAY FLAMES IN THE DLR GENERIC SINGLE SECTOR COMBUSTOR
EXPERIMENTAL INVESTIGATION OF LEAN BLOWOUT LIMITS OF A COMBUSTION-AIR-HEATER
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
FUEL SPRAY EFFECTS ON SELF-EXCITED COMBUSTION INSTABILITY IN A BLUFFBODY STABILIZED FLAME