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Exploratory flight investigation and analysis of structural loads encountered by a helicopter hingeless rotor systemFlight test and analysis of structural loads in helicopter hingeless rotor system
Document ID
19660030151
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ward, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3676
Accession Number
66N39441
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HELICOPTER
AERODYNAMIC LOAD
FLIGHT TEST
RIGID ROTOR HELICOPTER
ROTOR

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