Introducing students to selected topics of theoretical and experimental aerodynamic in hyposonic, subsonic, transonic, supersonic and hipersonic speed area.

Students will be introduced to the procedure of abstract thinking and creative idea generation,the methodology of the design and development of new aircraft and spacecraft on the most advanced technological solutions.

The characteristics in the subsonic, transonic, supersonic and hipersonic wind tunnel testing. Calculation methods in aerodynamics, Selected topics from the boundary layer theory and turbulent flow. The characteristics of flow at low Reynolds numbers.

Modeling and Simulation of flow with MATLAB, FLUENT etc. Simulation aerodynamic parameters in wind tunnels.

No special conditions.

Require additional materials (handouts, setting assignments, term papers, etc.) Are given at the web site or reproduced on paper. Large-scale electronic materials can be made available to students in direct contact.

Total assigned hours: 65

New material: 40
Elaboration and examples (recapitulation): 10

Auditory exercises: 0
Laboratory exercises: 0
Calculation tasks: 0
Seminar paper: 0
Project: 0
Consultations: 0
Discussion/workshop: 0
Research study work: 0

Review and grading of calculation tasks: 0
Review and grading of lab reports: 0
Review and grading of seminar papers: 5
Review and grading of the project: 0
Test: 0
Test: 0
Final exam: 10

Activity during lectures: 15
Test/test: 0
Laboratory practice: 0
Calculation tasks: 0
Seminar paper: 45
Project: 0
Final exam: 40
Requirement for taking the exam (required number of points): 45

H. Ashley: Aerodynamics of Wings and Bodies, McGraw Hill, 1995.; R. T. Jones, D. Cohen: High Speed Wing Theory, Princeton University Press, 1980.; J. Katz, A. Plotkin: Low Speed Aerodynamics from Wing Theory to Panel Method, McGraw-Hill Co., Singapore, 1991.; Б. Рашуо, Утицај зидова трансоничних аеротунела на аеродинамичка испитивања, Универзитет у Београду, Машински факултет, Београд, 1999.