2019
DOI: 10.1007/s42417-019-00085-5
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Experimental and Numerical Studies on Aerodynamic Control of NACA 4418 Airfoil with a Rotating Cylinder

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Cited by 9 publications
(5 citation statements)
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“…Stall appears at around 21 degrees in angle of attack for both HC and SC models. In fact, critical angle of attack for appearance of stall for the NACA 4418 airfoil was also found around 16 degrees [8]. However, surface imperfections and roughness can cause a flow separation, leading experimental stall angle to deviate from expected values [9].…”
Section: Aerodynamic Coefficientsmentioning
confidence: 95%
See 1 more Smart Citation
“…Stall appears at around 21 degrees in angle of attack for both HC and SC models. In fact, critical angle of attack for appearance of stall for the NACA 4418 airfoil was also found around 16 degrees [8]. However, surface imperfections and roughness can cause a flow separation, leading experimental stall angle to deviate from expected values [9].…”
Section: Aerodynamic Coefficientsmentioning
confidence: 95%
“…However, surface imperfections and roughness can cause a flow separation, leading experimental stall angle to deviate from expected values [9]. In addition, onset of stall also depends on Reynolds numbers [8].…”
Section: Aerodynamic Coefficientsmentioning
confidence: 96%
“…Table 1 shows information for 1 OPT blade with each section as in Figure 1 having its airfoil distance with different chord sizes and twist degrees. Due to its high lift and low drag coefficients, small HAWT blades frequently utilize the NACA 44xx and NACA 230xx family airfoils [21]. The NACA 4418 was employed in this study, with a maximum lift-to-drag ratio of 44.447, which equates to an angle of attack of 6.5° and a lift coefficient of 1.209.…”
Section: Methodology 21 Wind Turbine Specificationmentioning
confidence: 99%
“…The advantage of the NACA 4418 blade is to enhance the aerodynamic efficiency by its flow control behaviour. Also, this airfoil has the capability to improve the lift to drag ratio for certain wind directions and speed by varying the airfoil's thickness coefficients suitably (Lou et al 2020).…”
Section: Bend Diffuser Design With Intake Funnel Type Hopper Natural ...mentioning
confidence: 99%