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- 저자 : O. Žigo (검색결과 2 건)
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Z. Špitalský,D. Rástočná Illová,O. Žigo,M. Mičušík,Z. Nógellová,M. Procházka,A. Kleinová,M. Kováčová,I. Novák 한국섬유공학회 2019 Fibers and polymers Vol.20 No.8
Polyester (PES) fabrics were pre-treated with atmospheric discharge plasma, and the surface properties, chemicalcomposition, and physical changes on the surfaces of the PES fabrics were investigated. The hydrophobic recovery of theplasma-modified surface during aging of the PES fabrics treated with plasma was also investigated. The glycerin contactangles were determined along with the chemical composition changes in the PES fabric using X-ray photoelectronspectroscopy, Fourier-transform infrared spectroscopy, and iodometric analyses. The physical changes in the topography androughness of the plasma-modified PES were studied using scanning electron microscopy and nanoindentation. The relationbetween the hydrophilicity and hydroperoxide concentration on the surface of the plasma-treated PES fabrics was analyzedand the antibacterial behavior of the fabrics with respect to selected two bacterial strains was monitored.
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Design Optimization and Investigation of Aerodynamic Characteristics of Low Reynolds Number Airfoils
Arshad Ali,Rodrigues Lucas Brandão,López Iñigo Martínez 한국항공우주학회 2021 International Journal of Aeronautical and Space Sc Vol.22 No.4
This study aims to develop a simple and efficient design optimization methodology for the low Reynolds number airfoils. XFOIL is used as an aerodynamic solver while modeFRONTIER workflow is employed for the design optimization purpose. The airfoil SG6043 is used as the reference airfoil for optimization due to its common applications when long-endurance characteristics are desired. A simple design optimization methodology with the integration of XFOIL in the modeFRONTIER workflow environment is proposed in this study. The proposed “software integration methodology” demonstrated up to 10% improvement in the optimization parameter which makes it more efficient by reducing the optimization time and steps without unnecessary user intervention which are the limitations conventionally associated with the optimization process. The optimization results are further compared with the results of the numerical simulations. The use of the transition-sensitive turbulence model allowed the evaluation of the behavior of the laminar separation bubble for different angles of attack, observing that it shifts towards the leading edge and has its length reduced as the angle of attack increases. The newly generated airfoil exhibits improved aerodynamic characteristics as compared to the base airfoil. The optimized airfoil can be used in the applications of UAVs as well as in general aviation. Further validation of the airfoil using wind tunnel testing is recommended and planned.
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