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
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
IMPROVED CHEMICAL KINETIC MODEL REDUCTION IN PYMARS FOR LIQUID PROPELLANTS