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Rotorcraft dynamicsThe dynamic structural analysis of rotary winged aircraft is reported, considering helicopter vibration and loads.
Document ID
19740026376
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-SP-352
Accession Number
74N34489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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