DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
DEFINING A TESTBED FOR THE U.S. TURBINE INDUSTRY: THE NATIONAL EXPERIMENTAL TURBINE (NEXT)
MULTIDISCIPLINARY OPTIMIZATION OF A HELICOPTER GTE TURBINE
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
FLAME SPEED OF TURBULENT PREMIXED KERNEL IN TURBULENT FLOWS
DEVELOPMENT AND TESTING OF PULSE GUNS FOR COMBUSTION INSTABILITY TESTING
BROADBAND, MID-INFRARED LASER-ABSORPTION MEASUREMENTS OF TEMPERATURE, CH4, AND C3H8 IN FLAMES
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