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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