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
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR