Effect of Air-Flow Distribution and Total-Pressure Loss on Performance of One-Sixth Segment of Turbojet Combuster

Author: Hill, Francis U.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SE7K16
Link: https://digital.library.unt.edu/ark:/67531/metadc65249/

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