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
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR