NASA NTRS · 20100033605
Nonlinear Combustion Instability Prediction
Abstract
The liquid rocket engine stability prediction software (LCI) predicts combustion stability of systems using LOX-LH2 propellants. Both longitudinal and transverse mode stability characteristics are calculated. This software has the unique feature of being able to predict system limit amplitude.
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Flandro, Gary. 2010-09-01. Nonlinear Combustion Instability Prediction. https://ntrs.nasa.gov/citations/20100033605
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