4.5 Article

The scaling of rotor inertia under dynamic inflow conditions

Journal

JOURNAL OF FLUIDS AND STRUCTURES
Volume 106, Issue -, Pages -

Publisher

ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD
DOI: 10.1016/j.jfluidstructs.2021.103357

Keywords

Rotor aerodynamics; Moment of inertia; Unsteady environments; Gusts

Funding

  1. NSERC CREATE Sustainable Engineering in Remote Areas (SERA), Canada
  2. DER's NSERC Discovery Grant, Canada

Ask authors/readers for more resources

Rotor moment of inertia significantly affects the performance of rotating systems, and a normalized inertia number (I*) is introduced to characterize the dynamic response of a generic-rotor system relative to flow inertia. Experiments in a towing tank facility show that rotors with lower I* produce higher power output during gusts. Increasing I* and decreasing flow inertia result in a smaller increase in power output.
Rotor moment of inertia significantly influences the performance of rotating systems, such as wind and tidal turbines, when operating in unsteady environments. However, rotor moment of inertia in itself does not fully define the unsteady behaviour of such rotating systems without taking flow inertia, e.g. the gust acceleration, into consideration. We therefore introduce a normalized inertia number (I*), which relates the influence of rotor moment of inertia relative to the flow inertia in order to characterize the dynamic response of a generic-rotor system. Experiments are performed in a towing tank facility using three geometrically-identical rotor models with weighted tips so as to investigate the influence of I* on the rotor's ability to adapt to changing inflow conditions. Gust profiles with four gust durations were tested, ranging from slow quasi-steady operation to rapid disturbances. Rotors operating with sufficiently low I* are found to produce higher normalized power during the fastest tested gust when compared to the quasi-steady operation. For instance, the power output of the rotor model with (I* = 3.2 x 10(-3)) is, at its maximum, 30% higher during the fastest gust versus quasi-steady operation. However, by increasing I* on the same rotor model to 8.7 x 10(-3), by decreasing the flow inertia, the rotor model produced, at maximum, only 19% higher power output. Therefore, we are able to show that our normalization I* is a reasonable way to determine the dynamic performance of a rotating system during a gust. (C) 2021 Elsevier Ltd. All rights reserved.

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