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Acceptability of vtol aircraft noise determined by absolute subjective testingA program was conducted during which test subjects evaluated the simulated sounds of a helicopter, a tilt wing aircraft, and a 15 second, 90 PNdB (indoors) turbojet aircraft used as reference...
général - core.ac.uk - PDF: hdl.handle.net
Flow diverter value and flow diversion method... Examples of application of the flow diverter valve to a liquid rocket and a turbojet aircraft engine are given...
Nonlinear model predictive control of an aircraft gas turbine engine †The feasibility of constrained nonlinear model predictive control (NMPC) with state estimation is investigated and applied to a high-fidelity turbojet aircraft engine model...

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