naca-rm-e55l13a

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naca-rm-e55l13a Dynamics of a Supersonic Inlet with Adjustable Bypass in Combination with a J34 Turbojet Engine.pdfDownload 

National Advisory Committee for Aeronautics, Research Memorandum - Dynamics of a Supersonic Inlet with Adjustable Bypass in Combination with a J34 Turbojet Engine


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