2018
DOI: 10.2514/1.c035065
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Nacelle Strake Design for Short Takeoff and Landing Configuration with Turboprop Engines

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Cited by 4 publications
(1 citation statement)
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“…Considering propeller effects for the take-off configuration with maximum power condition (484 kW per propeller), the maximum effective lift coefficient is increased by ∆C L,max = 0.62 or 24 %. In order to further enhance C L,max under prop off conditions, nacelle strakes have been designed for nacelle 1 and nacelle 4 based on the experience from previous studies [16]. The impact of those strakes on the flowfield of the landing configuration at high angles of attack is demonstrated in figure 7…”
Section: Procedure Considerations and Constraintsmentioning
confidence: 99%
“…Considering propeller effects for the take-off configuration with maximum power condition (484 kW per propeller), the maximum effective lift coefficient is increased by ∆C L,max = 0.62 or 24 %. In order to further enhance C L,max under prop off conditions, nacelle strakes have been designed for nacelle 1 and nacelle 4 based on the experience from previous studies [16]. The impact of those strakes on the flowfield of the landing configuration at high angles of attack is demonstrated in figure 7…”
Section: Procedure Considerations and Constraintsmentioning
confidence: 99%