Propellant Spray Combustion Processes During Stable and Unstable Liquid Rocket Combustion
R. D. Sutton
Abstract:Information resulting from this study will allow formulation of new and very general analytical models and criteria to permit a priori design of reliable and stable liquid rocket motors and supersonic air-breathing engines required for future weapons delivery systems. From the test data drop diameterso, velocity and pressure wave growth or decay as a function nf chamber length and initial conditions will be determined. These data can then be input to appropriate newly deyeloped combustion models and the validi… Show more
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