AERODYNAMICS CALCULATION LAB.

Course objectives

The Lab of Computational Aerodynamics aims at: 1) Providing the students with a proper understanding of wing system aerodynamics. The related skills concern theoretical and numerical aspects, in particular: a) mathematical modeling of the external flow about wing systems; b) capability of dealing with and interpreting the meaning of the equations stemming from the mathematical model; c) knowledge of the basic discretization techniques used in external aerodynamics. 2) Provide the students with the ability to numerically predict the aerodynamic characteristics of wing systems. Specifically: a) The capability of correctly describing the geometry of the wing system; b) The ability to reproduce the relevant geometries in discrete form; c) The ability in using free-ware aerodynamic simulation tools to estimate the aerodynamic characteristics of wing systems; d) The capability of interpreting the results of numerical simulations in terms of flow field and force systems acting on the wing. 3) Develop the ability of critically selecting and assessing the numerical tools most appropriate for solving problems in aerodynamics and interpret and understand the results of the relevant numerical solution, also by comparison with experimental results.

Channel 1
CARLO MASSIMO CASCIOLA Lecturers' profile

Program - Frequency - Exams

Course program
1. Potential flows. 2. Boundary integral representations for potential flows. 3. Green function. 4. Integral representation for the aerodynamic field. 5. Boundary integral equation for aerodynamics. 6. Discretization techniques for boundary integral equations. 7. Panel methods for two-dimensional flows. 8. The Vortex Lattice Method for three-dimensional flows. 9. Freeware for two dimensional aerodynamics. 10. Freeware for three dimensional aerodynamics. 11. Aerodynamics characteristics of wing systems.
Prerequisites
Good knowledge of calculus and basic understanding of differential equations. Good understanding of mechanics, basic physics and thermodynamics. Good knowledge of aerodynamics and fluid dynamics.
Books
Lecture notes provided by the teacher.
Teaching mode
The lectures are organized in two complementary sections aimed at completing the student theoretical background and practical/technical skills in aerodynamic computations. The first part consists of lectures/seminars delivered by teacher and collaborators to recall aerodynamics fundamentals and complementary notions necessary for a clear understanding of the basic computational technics in aerodynamics. The second part is devoted to hands on sessions to allow the students developing computational skills and a critical attitude towards the numerical results.
Frequency
Although not mandatory, attendance to class lecture is warmly encouraged.
Exam mode
The final evaluation is based on the quality, clarity, completeness and accuracy of a report presented by the student concerning the results of the aerodynamic computation of an aerodynamic configuration of her/his own interest.
Lesson mode
The lectures are organized in two complementary sections aimed at completing the student theoretical background and practical/technical skills in aerodynamic computations. The first part consists of lectures/seminars delivered by teacher and collaborators to recall aerodynamics fundamentals and complementary notions necessary for a clear understanding of the basic computational technics in aerodynamics. The second part is devoted to hands on sessions to allow the students developing computational skills and a critical attitude towards the numerical results.
  • Lesson codeAAF1312
  • Academic year2025/2026
  • CourseAerospace engineering
  • CurriculumSingle curriculum
  • Year3rd year
  • Semester2nd semester
  • CFU3