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Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model /

Bibliographic Details
Main Authors: Csank, Jeffrey T., (Author), Stueber, Thomas J., (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.), (sponsoring body.)
Format: Government Document Online Book
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
Series:NASA technical memorandum ; 216515.
Online Access:ONLINE VERSION
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