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Unformatted text preview: Course Syllabus AE443 - COMPUTATIONAL AERODYNAMICS Instructor : Dr. ISMAIL H. TUNCER E-Mail : email@example.com Phone : 210-4289 DESCRIPTION Simplifications to the Navier-Stokes equations for steady, attached flows. Integral formulation of potential flow equations for subsonic flows. Potential flow solutions with panel methods. Gradient based design optimization, inverse airfoil design using a panel method. Full potential flow equation, characteristic lines, analysis of transonic potential flows past airfoils based on the Transonic Small Disturbance (TSD) equation, upwind differencing in supersonic flow regions, Numerical solution of the TSD equation using Finite Difference methods. Numerical solution of the Full Potential flow Equation (FPE), coordinate transformations, discretization of FPE equation in curvilinear coordinate systems. REQUIREMENTS • AE305, AE341, and the consent of the instructor • Fluency in Fortran programming • Experience in data processing with graphical output using...
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- Spring '11