Modeling of Liquid Jet Atomization Processes.
Final technical rept. 1 Jul 94-30 Jun 96,
PURDUE UNIV LAFAYETTE IN SCHOOL OF AERONAUTICS AND ASTRONAUTICS
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This report summarizes atomization simulations performed to investigate the role of this process in liquid rocket engine combustion instabilities. The research involves the development and application of a series of nonlinear free surface models based on boundary element methods B EMs. Models have been developed to study the effects of unsteady injection, transverse acoustic wave interactions such as those experienced in the F-1 engine, longitudinal acoustic wave interactions, and the dynamics of droplets in the presence of an acoustic wave. Results for each of these four models is presented in this document.
- Operations Research
- Combustion and Ignition
- Solid Propellant Rocket Engines