In previous work, the effects of power extraction for onboard electrical equipment and flight control systems were studied to determine which turbine shaft (i.e. high power shaft vs low power shaft) is best suited for power extraction. This thesis will look into an alternative option, a three-spool design with a high-pressure turbine, low-pressure turbine, and a turbine dedicated to driving the fan. One of the three-spool turbines is designed to be a vaneless counter-rotating turbine.
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- Partial requirement for: M.S., Arizona State University, 2019Note typethesis
- Includes bibliographical references (pages 63-64)Note typebibliography
- Field of study: Aerospace Engineering