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Rotor blade dynamic designThe rotor dynamic design considerations are essentially limitations on the vibratory response of the blades which in turn limit the dynamic excitation of the fuselage by forces and moments transmitted to the hub. Quantities which are associated with the blade response and which are subject to design constraints are discussed. These include blade frequencies, vertical and inplane hub shear, rolling and pitching moments, and aeroelastic stability margin.
Document ID
19900003267
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pritchard, Jocelyn I. (NASA Langley Research Center Hampton, VA, United States)
Adelman, Howard M. (NASA Langley Research Center Hampton, VA, United States)
Mantay, Wayne R. (Army Aviation Systems Command Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1989
Publication Information
Publication: Integrated Multidisciplinary Optimization of Rotorcraft: A Plan for Development
Subject Category
Aircraft Design, Testing And Performance
Accession Number
90N12583
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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