A Turbosail profile analysis code based on the panel method

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• 作者：Cherif Hcini^a ; ^{hcinicherif@hotmail.com} ; Essia Abidi^a ; Badreddine Kamoun^a ; David Afungchui^b
• 关键词：Turbosail ; Panel method ; Suction ; Flap ; Lift ; Drag
• 刊名：Energy
• 出版年：2017
• 出版时间：1 January 2017
• 年：2017
• 卷：118
• 期：Complete
• 页码：147-155
• 全文大小：946 K
• 卷排序：118

文摘

A numerical model of the air flow around the Turbosail profile is presented. Panel method is used. The effect of the relative thickness of Turbosail profile on aerodynamic performance is explored. The influence of the flap angle and the suction on the lift and drag coefficients are studied. Results are very important for developing the simple design and applications for Turbosail.