naca-rm-e6i20

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naca-rm-e6i20 Altitude Wind Tunnel Investigation of Thrust Augmentation of a Turbojet Engine - I - Performance with Tail-Pipe Burning.pdf  Download  

National Advisory Committee for Aeronautics, Research Memorandum - Altitude Wind Tunnel Investigation of Thrust Augmentation of a Turbojet Engine - I - Performance with Tail-Pipe Burning


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