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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.05.031
Abstract: Abstract Thrust control in aero-engines is achieved indirectly due to the lack of thrust sensing technologies. A related variable must be chosen for the control, typically high or low pressure rotor speeds. In this paper,…
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Keywords:
rotor;
aero;
lpv model;
control aero ... See more keywords