2017
DOI: 10.2514/1.c033870
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Wind-Turbine Wake Encounter by Light Aircraft

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Cited by 4 publications
(11 citation statements)
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“…Conversely, our results using an actuator-line representation of a wind turbine in the SOWFA LES model never surpass the low roll hazard threshold. Rather, our results agree with those of Wang et al (2015Wang et al ( , 2017, whose calculations are computed from the Beddoes circulation formula (Madsen and Rasmussen, 2004), as opposed to the wind tunnel extrapolation in Mulinazzi and Zheng (2014). Past successes in 20 turbine wake modeling using LES actuator-line methods can in part validate our results (e.g., Churchfield et al (2012);Nilsson et al (2015); Jha et al (2015)).…”
supporting
confidence: 79%
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“…Conversely, our results using an actuator-line representation of a wind turbine in the SOWFA LES model never surpass the low roll hazard threshold. Rather, our results agree with those of Wang et al (2015Wang et al ( , 2017, whose calculations are computed from the Beddoes circulation formula (Madsen and Rasmussen, 2004), as opposed to the wind tunnel extrapolation in Mulinazzi and Zheng (2014). Past successes in 20 turbine wake modeling using LES actuator-line methods can in part validate our results (e.g., Churchfield et al (2012);Nilsson et al (2015); Jha et al (2015)).…”
supporting
confidence: 79%
“…5) is calculated for an aircraft inside and outside the wake for the neutral (Figure 4b) and stable ( Figure 4d) cases to categorize each moment as a "low", "medium", or "high" hazard as used in the Mulinazzi and Zheng (2014) and Wang et al (2015) assessments of wake roll 20 hazards. These assessment criteria are based on the maximum rolling moment that the aileron on a typical aircraft can generate to counteract a moment induced by the wake field (Wang et al, 2015). A wake-induced rolling moment coefficient |C roll | above 0.28 is considered a high hazard, between 0.1 and 0.28 a medium hazard, and below 0.1 a low hazard.…”
Section: Resultsmentioning
confidence: 99%
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