Experimental investigation on the Langley helicopter test tower of compressibility effects on a rotor having NACA 63₂-015 airfoil sections

Author: Shivers, James P.
Year: 1956
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3850
Link: https://digital.library.unt.edu/ark:/67531/metadc56145/

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