1	Course Title:	AERODYNAMIC
2	Course Code:	MAK4311sil
3	Type of Course:	Optional
4	Level of Course:	First Cycle
5	Year of Study:	4
6	Semester:	7
7	ECTS Credits Allocated:	4
8	Theoretical (hour/week):	3
9	Practice (hour/week) :	0
10	Laboratory (hour/week) :	0
11	Prerequisites:	-
12	Recommended optional programme components:	None
13	Language:	Turkish
14	Mode of Delivery:	Face to face
15	Course Coordinator:	Dr. Ögr. Üyesi ONUR YEMENİCİ
16	Course Lecturers:	-
17	Contactinformation of the Course Coordinator:	oseckin@uludag.edu.tr / 2242940910 / U.Ü. Müh. Fak. Mak. Müh. Bölümü BURSA
18	Website:
19	Objective of the Course:	To give the fundamentals of incompressible aerodynamics and to solve basic aerodynamics problems.
20	Contribution of the Course to Professional Development

21

Learning Outcomes:

1 Know the basic equations for inviscid incompressible flow ; 2 Find the potential and stream functions for the flow around bosies and calculate the pressure distribution ; 3 Calculate the lift and moment coefficients by using thin airfoil theory; 4 Calculate the lift and drag for finite wings at different planforms;

22	Course Content:

Week	Theoretical	Practical
1	Aerodynamic forces and moments
2	Dimensional analysis and similarity
3	Models of the fluids, continuity and momentum equations, Drag of a 2-D body
4	Fundamental equations of flow, pathlines, streamlines, streaklines
5	Stream function, velocity potential, fundamentals of inviscid incompressible flow
6	Bernoulli's equation, pitot tube
7	Laplace's equation, uniform flow, source and doublet flows, flow over a circular cylinder
8	Vortex flow, Lifting flow over a cylinder, Kutta Joukowski theorem
9	I. Midterm exam
10	Incompressible flows over airfoils, Kutta condition, Kelvin's circulation theorem
11	Thin airfoil theory, symmetric and cambered airfoils
12	Incompressible flow over finite wings, downwash and induced drag,the vortex flament, the Biot-Savart Law and Helmholtz theorems
13	Panel methods, lifting line theory, elliptical lift distribution
14	General lift distribution, effect of aspect ratio

23	Textbooks, References and/or Other Materials:	1. Anderson, J.D., 2001, Fundamentals of Aerodynamics, McGraw-Hill. 2. Houghton, E.L. and Carpenter, P.W., 2003, Aerodynamics for Engineering Students, Butterworth-Heinemann. 3. Bertin, J.J and Smith, M.L., 2008, Aerodynamics for Engineers, Prentice-Hall.
24	Assesment

TERM LEARNING ACTIVITIES	NUMBER	PERCENT
Midterm Exam	1	35
Quiz	0	0
Homeworks, Performances	1	15
Final Exam	1	50
Total	3	100
Contribution of Term (Year) Learning Activities to Success Grade		50
Contribution of Final Exam to Success Grade		50
Total		100
Measurement and Evaluation Techniques Used in the Course
Information

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ECTS / WORK LOAD TABLE

Activites	NUMBER	TIME [Hour]	Total WorkLoad [Hour]
Theoretical	14	3	42
Practicals/Labs	0	0	0
Self Study and Preparation	14	4	56
Homeworks, Performances	1	14	14
Projects	0	0	0
Field Studies	0	0	0
Midtermexams	1	4	4
Others	0	0	0
Final Exams	1	4	4
Total WorkLoad			120
Total workload/ 30 hr			4
ECTS Credit of the Course			4

26	CONTRIBUTION OF LEARNING OUTCOMES TO PROGRAMME QUALIFICATIONS
PQ1 PQ2 PQ3 PQ4 PQ5 PQ6 PQ7 PQ8 PQ9 PQ10 PQ11 PQ12 PQ13 PQ14 LO1 2 2 0 0 0 0 4 0 0 0 0 0 0 0 LO2 4 4 0 2 0 0 4 0 0 0 0 0 0 0 LO3 4 4 0 0 0 0 4 0 0 0 0 0 0 0 LO4 0 0 0 0 0 0 0 0 0 0 0 0 0 0

LO: Learning Objectives

PQ: Program Qualifications

Contribution Level:

1 Very Low

2 Low

3 Medium

4 High

5 Very High