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COMPUTATIONAL AERODYNAMICS COURSE IDENTIFICATION AND APPLICATION INFORMATION

Code Name of the Course Unit Semester In-Class Hours (T+P) Credit ECTS Credit
UCK446 COMPUTATIONAL AERODYNAMICS 5 3 3 5

KEY LEARNING OUTCOMES OF THE COURSE UNIT (On successful completion of this course unit, students/learners will or will be able to)

Understand 2- and 3-dimensional potential flow problems, modeling them with integral equations and boundary conditions, Learn to solve the thin profile problem with the clustered vortices method, Learn to solve the airfoil problem with the surface singularities method, Learn to solve the finite wing problem with the vortex lattice method, Learn to solve an aircraft fuselage problem with the panel method, Understand how to solve the time-dependent problem for airfoils with the surface singularities method.