NASA NTRS · 19900003267
Rotor blade dynamic design
Abstract
The 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.
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Pritchard, Jocelyn I., Adelman, Howard M., Mantay, Wayne R.. 1989-05-01. Rotor blade dynamic design. https://ntrs.nasa.gov/citations/19900003267
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