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A physics-based emissions model for aircraft gas turbine combustors
(Massachusetts Institute of Technology, 2006)
In this thesis, a physics-based model of an aircraft gas turbine combustor is developed for predicting NO. and CO emissions. The objective of the model is to predict the emissions of current and potential future gas turbine ...
Uncertainty assessment of complex models with application to aviation environmental systems
(Massachusetts Institute of Technology, 2009)
Numerical simulation models that support decision-making and policy-making processes are often complex, involving many disciplines, and long computation times. These models typically have many factors of different character, ...