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Low tip Mach number stall characteristics and high tip Mach number compressibility effects on a helicopter rotor having an NACA 0009 tip airfoil section
Author:
Powell, Robert D., Jr.
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4355
Link:
https://digital.library.unt.edu/ark:/67531/metadc57385/
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