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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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