DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS
Bahbah, M., Abdel Azim, A. (1991). DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS. EKB Journal Management System, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), 1-13. doi: 10.21608/asat.1991.25657
Mohamed M. Bahbah; Ahmed F. Abdel Azim. "DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS". EKB Journal Management System, 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, 1991, 1-13. doi: 10.21608/asat.1991.25657
Bahbah, M., Abdel Azim, A. (1991). 'DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS', EKB Journal Management System, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), pp. 1-13. doi: 10.21608/asat.1991.25657
Bahbah, M., Abdel Azim, A. DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS. EKB Journal Management System, 1991; 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO): 1-13. doi: 10.21608/asat.1991.25657

DEVELOPMENT OF A PANEL METHOD FCR THE STUDY CF TWO-DIMEN-SIONAL POTENTIAL FLOG OVER SINGLE AND TWO-ELEMENT AIRFOILS

International Conference on Aerospace Sciences and Aviation Technology
Article 1, Volume 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, May 1991, Page 1-13  XML PDF (1.93 MB)
Document Type: Original Article
DOI: 10.21608/asat.1991.25657
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Authors
Mohamed M. Bahbah1; Ahmed F. Abdel Azim2
1Lecturer, Aeronouticol Engineering Dept., Al-Fcteh University, Tripoli-Libya.
2Associate Professor, Aeronouticol Engineering Dept., Al-Fcteh University, Tripoli-Libya.
Abstract
Panel methods proved a powerful-numerical method capable for hand-ling both internal and external flows. In this paper a vortex panel method is employed for studying the potential flow over one and two-element airfoils. A second order vortex method is developed to overcome the instability found in the solution when a first order vortex method is employed. Three different methods for panelling are suggested. The effect of the number of panels is also examined. Comparison of the results obtoined by this model and the exact solution of Williams two-element airfoil proved its validity. The effects of the gap and the overlap in the case of two-element air-foil are examined.
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