NASA NTRS · 20080005933
Aircraft thrust control
Abstract
An integrated control system for coaxial counterrotating aircraft propulsors driven by a common gas turbine engine. The system establishes an engine pressure ratio by control of fuel flow and uses the established pressure ratio to set propulsor speed. Propulsor speed is set by adjustment of blade pitch.
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Walker, Neil, Day, Stanley G., Collopy, Paul D., Bennett, George W.. 1988-09-20. Aircraft thrust control. https://ntrs.nasa.gov/citations/20080005933
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