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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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