3 edition of Helicopter far-field acoustic levels as a function of reduced main-rotor advancing blade-tip Mach number found in the catalog.
Helicopter far-field acoustic levels as a function of reduced main-rotor advancing blade-tip Mach number
by National Aeronautics and Space Administration, Langley Research Center in Hampton, Va
Written in English
|Other titles||Helicopter far field acoustic levels ....|
|Statement||Arnold W. Mueller, Charles D. Smith, and Phillip LeMasurier.|
|Series||NASA technical memorandum -- 102684.|
|Contributions||Smith, Charles D., 1936-, LeMasurier, Phillip., Langley Research Center.|
|The Physical Object|
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