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Performance of Compressor of XJ-41-V Turbojet Engine 2 - Static-Pressure Ratios and Limitation of Maximum Flow at Equivalent Compressor Speed of 8000 RPM
Author:
Dildine, Dean M.
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E7E05
Link:
https://digital.library.unt.edu/ark:/67531/metadc65002/
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