Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 3 - Analysis of Combustion-Chamber Performance

Author: Campbell, Carl E.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E8B19
Link: https://digital.library.unt.edu/ark:/67531/metadc63848/

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