On the Kutta Condition in Potential Flow over Airfoil. (8th April 2014)

• Record Type: Journal Article
• Authors: Mohebbi, Farzad; Sellier, Mathieu
• Other Names: Saha Ujjwal K. Academic Editor.
• Is Part Of: Journal of aerodynamics. Volume 2014(2014)
• Publication Date: 2014-04-08
• Subjects: Aerodynamics -- Periodicals; Aerodynamics; Periodicals; 533.62
• DOI: 10.1155/2014/676912
• Languages: English
• ISSNs: 2356-7139

Abstract

Abstract : This paper proposes a novel method to implement the Kutta condition in irrotational, inviscid, incompressible flow (potential flow) over an airfoil. In contrast to common practice, this method is not based on the panel method. It is based on a finite difference scheme formulated on a boundary-fitted grid using an O-type elliptic grid generation technique. The proposed algorithm uses a novel and fast procedure to implement the Kutta condition by calculating the stream function over the airfoil surface through the derived expression for the airfoils with both finite trailing edge angle and cusped trailing edge. The results obtained show the excellent agreement with the results from analytical and panel methods thereby confirming the accuracy and correctness of the proposed method.