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Reduced Basis and Stochastic Modeling of Liquid Propellant Rocket Engine as a Complex System
Technical Report,01 Jun 2012,30 May 2015
UNIVERSITY OF CALIFORNIA IRVINE IRVINE
Pagination or Media Count:
The four-institution research team has developed a framework for stochastic analysis of nonlinear combustion instability with triggering and in the use of reduced-basis models RBM, large-eddy simulations, and multi-scale asymptotic models for the analysis. Results published during these three years and ongoing researches are briefly discussed and addenda with more detail are provided.
APPROVED FOR PUBLIC RELEASE