NASA NTRS · 19740035390
An unsteady wake model for a hingeless rotor
Abstract
A simple nonsteady wake model derived from the unsteady moment of the momentum equation for zero advance ratio is correlated with cyclic pitch frequency response tests conducted with a small hingeless rotor model. Two and three or more bladed rotor analyses are presented.
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Crews, S. T., Hohenemser, K. H., Ormiston, R. A.. 1973-12-01. An unsteady wake model for a hingeless rotor. https://ntrs.nasa.gov/citations/19740035390
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