سال انتشار: ۱۳۹۰

محل انتشار: اولین کنفرانس بین المللی رویکردهای نوین در نگهداشت انرژی

تعداد صفحات: ۹

نویسنده(ها):

karar hajagha – a Mechanic PHD Student Isfahan University of Technology
mehdi jahangiri – a Mechanic PHD Student Isfahan University of Technology
ahmad sedaghat – Department of Mechanical Engineering Isfahan University of Technology, Isfahan,

چکیده:

In this paper theoretical analysis of six airfoils, the AG24, AG35, AG455ct, CAL1215j, CAL2263m and CAL4041l has been done. The analysis performed in this study are intended to provide theoretical predictions for power coefficient by used of MATLAB software based on experimental measurements at low Reynolds number. The results show that the airfoil appropriate to the design is AG35Airfoil.