Description

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.

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Date Created
2019
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  • Text
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    Note
    • Partial requirement for: M.S., Arizona State University, 2019
      Note type
      thesis
    • Includes bibliographical references (pages 63-64)
      Note type
      bibliography
    • Field of study: Aerospace Engineering

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    by Luke Micheal Burgett

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