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