High Speed Aerodynamics

ID: 0950
Course type: theoretical and methodological
Course coordinator: Kostić A. Ivan
Lecturers: Kostić A. Ivan, Kostić P. Olivera
Contact: Kostić A. Ivan
Level of studies: M.Sc. (graduate) Academic Studies – Mechanical Engineering
ECTS: 6
Final exam type: written
Department: Department of Aerospace Engineering

Lectures

Goal

The aim of this course is to introduce students to basic concepts of high speed aerodynamics. Emphasis is given to transonic and supersonic flow problems. External flows (supersonic airfoils, wings and complete aircraft lifting configurations) and internal flows (supersonic intakes, nozzles and diffusers).

Outcome

Upon completion and passing the course the student should be capable of understanding the basic concepts and problems in the field of aerodynamics at transonic and supersonic speeds. It is expected that the student knows how to apply the acquired knowledge in this field to solve practical engineering problems.

Theoretical teaching

The theoretical part of the course covers the following topics: Classification of flow and flow model (Navier-Stokes equations, the Euler, the potential of small disturbances, Prandtl-Glauert and Laplace). Singularities and discontinuities in the flow field. The method of characteristics and conical flow field. Airfoil in transonic and supersonic field (linear airfoil theory and the theory of higher order). Wing in supersonic flow (influence of tips, sweep, delta wing, supersonic and subsonic leading edge). Computational analysis of complete aircraft lifting configurations in transonic and supersonic flow fields. Intakes, nozzles and diffusers.

Practical teaching

Practical part of course demonstrates numerical examples in all areas. Practical work of students is accomplished through a virtual classroom, available 24 hours (program MOODLE). In the workshop students have access to the professor's lectures (handouts) and tests for practice. Practical training includes preparation of three projects. Each student works individually, and student qualifies for the final exam after completing at least two of the three projects.

Attendance requirement

Attended course in Applied Aerodynamics, or a course in fluid mechanics which provides satisfactory background knowledge (with professor’s approval).

Resources

The students have access to the virtual classroom on the Internet. At the first lecture students are enrolled and trained for work (Moodle software). In the workshops students have access to the lectures and exercises, guidelines for project preparation, internet resources, etc.

Assigned hours

Total assigned hours: 75

Active teaching (theoretical)

New material: 20
Elaboration and examples (recapitulation): 10

Active teaching (practical)

Auditory exercises: 10
Laboratory exercises: 0
Calculation tasks: 10
Seminar paper: 0
Project: 10
Consultations: 0
Discussion/workshop: 0
Research study work: 0

Knowledge test

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

Knowledge test (100 points total)

Activity during lectures: 10
Test/test: 30
Laboratory practice: 0
Calculation tasks: 0
Seminar paper: 0
Project: 30
Final exam: 30
Requirement for taking the exam (required number of points): 25

Literature

I. Kostić, O. Kostić: High Speed Aerodynamics, Handouts, University of Belgrade, Faculty of Mechanical Engineering, Belgrade 2023.; R. T. Jones: High Speed Wing Theory, Princeton University press, 1999.; H. Ashley: Aerodynamics of Wings and Bodies, McGraw Hill, 1995.