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An investigation of full-scale helicopter rotors at high advance ratios and advancing tip Mach numbersTabulated performance data of full-scale rotary wings at high advance ratios and advancing tip Mach numbers based on wind tunnel tests
Document ID
19680018796
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Biggers, J. C. (NASA Ames Research Center Moffett Field, CA, United States)
Mc Cloud, J. L., III (NASA Ames Research Center Moffett Field, CA, United States)
Stroub, R. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4632
Report Number: NASA-TN-D-4632
Accession Number
68N28268
Funding Number(s)
CONTRACT_GRANT: 721-01-00-13-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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