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• W2402122912 endingPage "795" @default.
• W2402122912 startingPage "757" @default.
• W2402122912 abstract "ABSTRACT An experimental validation of an optimised wing geometry in the Price-Païdoussis subsonic wind tunnel is presented. Two wing models were manufactured using optimised glass fibre composite and tested at three speeds and various angle-of-attack. These wing models were constructed based on the original aerofoil shape of the ATR 42 aircraft and an optimised version of the same aerofoil for a flight condition of Mach number equal to 0.1 and angle-of-attack of 0°. The aerofoil's optimisation was realised using an ‘in-house’ genetic algorithm coupled with a cubic spline reconstruction routine, and was analysed using XFoil aerodynamic solver. The optimisation was concentrated on improving the laminar flow on the upper surface of the wing, between 10% and 70% of the chord. XFoil-predicted pressure distributions were compared with experimental data obtained in the wind tunnel. The transition position was estimated from the experimental pressure data using a second derivative methodology and was compared with the transition predicted by XFoil code. The results have shown the agreement between numerical and experimental data. The wind-tunnel tests have shown that the improvement of the laminar flow of the optimised wing is higher than the value predicted numerically." @default.
• W2402122912 created "2016-06-24" @default.
• W2402122912 creator A5001815071 @default.
• W2402122912 creator A5021981211 @default.
• W2402122912 creator A5084087892 @default.
• W2402122912 date "2016-05-01" @default.
• W2402122912 modified "2023-10-16" @default.
• W2402122912 title "Numerical and experimental validation of a morphed wing geometry using Price-Païdoussis wind-tunnel testing" @default.
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• W2402122912 doi "https://doi.org/10.1017/aer.2016.30" @default.
• W2402122912 hasPublicationYear "2016" @default.
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