1. Airfoil Lift and Drag Extrapolation with Viterna and Montgomerie Methods
- Author
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Faisal Mahmuddin, Husni Sitepu, Surya Hariyanto, and Syerly Klara
- Subjects
Airfoil ,Lift-to-drag ratio ,Engineering ,Angle of attack ,business.industry ,Propeller (aeronautics) ,Computation ,Extrapolation ,02 engineering and technology ,Mechanics ,Structural engineering ,01 natural sciences ,010305 fluids & plasmas ,020303 mechanical engineering & transports ,0203 mechanical engineering ,0103 physical sciences ,Range (statistics) ,business ,Aerodynamic center - Abstract
In order to compute the performance of a propeller blade using blade element momentum (BEM) method, the two- dimensional airfoil performance of the propeller blade in terms of lift and drag coefficients is necessary. Such data usually can be obtained from model experiment only for limited range of angle of attack (AoA). Therefore, it is necessary to extrapolate the limited experimental data to obtain the data for the whole range of AoA. The present study uses 2 (two) methods which are Viterna and Montgomerie methods in order to extrapolate the performance of an airfoil. The formulas and procedures of both methods are presented and their application are also demonstrated using an airfoil shape of NACA23012. From this study, a relatively good agreement of the airfoil performance in terms of lift and drag coefficients can be found from computation results of the both methods.
- Published
- 2017
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