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Effect of Taper Configuration on the Aerodynamic Load Distribution and Efficiency of Wings in Steady Flow.

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Title: Effect of Taper Configuration on the Aerodynamic Load Distribution and Efficiency of Wings in Steady Flow.
Alternate Title: Daimî Akışta Trapez Kanat Konfigürasyonunun Kanatların Aerodinamik Yük Dağılımına ve Verimliliğine Etkisi.
Authors: Son, Onur1 onurson@gtu.edu.tr
Source: Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi. Jan2025, Vol. 18 Issue 1, p43-60. 18p.
Database: Academic Search Ultimate
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      – Code: eng
        Text: English
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        PageCount: 18
        StartPage: 43
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      – TitleFull: Effect of Taper Configuration on the Aerodynamic Load Distribution and Efficiency of Wings in Steady Flow.
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              Text: Jan2025
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              Y: 2025
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