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Published in 2018 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2018.11.094
Abstract: Abstract This paper proposes a complete robust control design procedure for combustion systems, present in a wide range of important applications. Using a non-linear model identified through optical instrumentation, it is proposed a linear model…
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Keywords:
output feedback;
optical instrumentation;
control;
feedback control ... See more keywords
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Published in 2021 at "ISA transactions"
DOI: 10.1016/j.isatra.2021.03.023
Abstract: This paper proposes a new filtering scheme applied to a linearized model of a nonlinear representation for combustion systems, whose parameters are obtained by means of optical sensors. To ensure a robust representation regarding the…
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Keywords:
combustion;
approach filtering;
instrumentation;
filtering combustion ... See more keywords
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Published in 2022 at "Entropy"
DOI: 10.3390/e24040564
Abstract: The entropy generation analysis of adiabatic combustion systems was performed to quantify the exergy losses which are mainly the exergy destroyed during combustion inside the chamber and in the exhaust gases. The purpose of the…
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Keywords:
exergy losses;
combustion systems;
combustion;
exhaust gas ... See more keywords
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Published in 2022 at "Entropy"
DOI: 10.3390/e24081099
Abstract: This paper provides a review of different contributions dedicated thus far to entropy generation analysis (EGA) in turbulent combustion systems. We account for various parametric studies that include wall boundedness, flow operating conditions, combustion regimes,…
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Keywords:
generation;
combustion systems;
generation analysis;
entropy generation ... See more keywords
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Published in 2017 at "Energies"
DOI: 10.3390/en10111900
Abstract: Through Computational Fluid Dynamics and validation, an optimal scramjet combustor has been designed based on twin-strut Hydrogen injection to sustain flight at a desired speed of Mach 8. An investigation undertaken into the efficacy of…
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Keywords:
supersonic combustion;
systems sustained;
combustion;
modeling supersonic ... See more keywords