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)
DEVELOPMENT AND TESTING OF PULSE GUNS FOR COMBUSTION INSTABILITY TESTING