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Bibliografiske detaljer
Format: Bog
Sprog:engelsk
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format Book
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id 0ebee124-6faa-4395-941d-e6cef6ffe890
isbn
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language eng
physical 1 online resource (17 pages) :color illustrations.
publication – publisher: National Aeronautics and Space Administration Glenn Research Center
  dateOfPublication: 2013
publishDate 2013
subjects
title Shock position control for mode transition in a turbine based combined cycle engine inlet model / Jeffrey T. Csank and Thomas J. Stueber.
topic Computerized simulation.
Engine inlets.
Feedback control.
Inlet flow.
Turbine engines.
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