Wind-tunnel tests of a full-scale helicopter rotor with symmetrical and with cambered blade sections at advance ratios from 0.3 to 0.4

Author:	McCloud, John L., III
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4367
Link:	https://digital.library.unt.edu/ark:/67531/metadc57455/