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Course Information
Course Unit Title : VISCOUS FLOW THEORY
Course Unit Code : 01MAK5172
Type of Course Unit : Optional
Level of Course Unit : Second Cycle
Year of Study : 1
Semester : 1.Semester
Number of ECTS Credits Allocated : 6,00
Name of Lecturer(s) : ---
Course Assistants : ---
Learning Outcomes of The Course Unit : 1) an ability to use knowledge of mathematics, science and engineering
2) an ability to design and conduct experiments as well as to analyze and interpret data
3) an ability to function on multidisciplinary teams
4) an ability to identify, formulate and solve engineering problems
5) an understanding of professional and ethical responsibility
6) an ability to communicate effectively
7) an ability to use the techniques and modern engineering tools necessary for engineering practice.
Mode of Delivery : Face-To-Face
Prerequisities and Co-requisities Courses : Unavailable
Recommended Optional Programme Components : Unavailable
Course Contents : This course is concerned with the introduction, unsteady viscous flows, three-dimensional boundary layers, compressible boundary layers, and hypersonic boundary layers.
Languages of Instruction : Turkish
Course Goals : This course will be helping to our students in engineering heat and fluid problems.
Course Aims : Our graduates will be successful in careers that deal with the design, simulation and analysis of engineering problems, experimentation and testing, manufacturing, and research.
WorkPlacement   Not Available
Recommended or Required Reading
Textbook :
Additional Resources : 1. Schlichting, H.: Boundary Layer Theory, McGraw Hill, 1979. 2. White, F. M.: Viscous Flow Theory, McGraw Hill, 1974. 3. Moore, F. K. (Editor): Theory of laminar Flows, High Speed Aerodynamics and Jet Propulsion Series, vol. 4, Princeton University Press, 1954. 4. Telionis, D. P.: Unsteady Viscous Flows, Springer-Verlag, 1981. 5. Hayes, W. D. And Probstein, R. F.: Hypersonic Flow Theory, Academic press, 1961.
Material Sharing
Documents :
Assignments :
Exams :
Additional Material :
Planned Learning Activities and Teaching Methods
Lectures, Practical Courses, Presentation, Seminar, Project, Laboratory Applications (if necessary)
ECTS / Table Of Workload (Number of ECTS credits allocated)
Student workload surveys utilized to determine ECTS credits.
Activity :
Number Duration Total  
Course Duration (Excluding Exam Week) :
13 3 39  
Time Of Studying Out Of Class :
13 5 65  
Homeworks :
10 5 50  
Presentation :
5 1 5  
Project :
0 0 0  
Lab Study :
0 0 0  
Field Study :
0 0 0  
Visas :
1 10 10  
Finals :
1 10 10  
Workload Hour (30) :
30  
Total Work Charge / Hour :
179  
Course's ECTS Credit :
6      
Assessment Methods and Criteria
Studies During Halfterm :
Number Co-Effient
Visa :
1 70
Quiz :
12 10
Homework :
5 15
Attendance :
0 5
Application :
0 0
Lab :
0 0
Project :
0 0
Workshop :
0 0
Seminary :
0 0
Field study :
0 0
   
TOTAL :
100
The ratio of the term to success :
40
The ratio of final to success :
60
TOTAL :
100
Weekly Detailed Course Content
Week Topics  
1 Introduction: A- Fundamental Equations for Viscous Flows B- Non-dimensionalization
 
2 Introduction: C- Boundary Layer Equations D- Review of Steady, Incompressible, 2-D Boundary Layer Theory
 
3 Unsteady Viscous Flows: A- Impulsively Started Flows B- Oscillatory Flows
 
4 Unsteady Viscous Flows: C- Unsteady Boundary Layer Separation
 
5 Three-Dimensional Boundary Layers: A- Boundary Layer Equations
 
6 Three-Dimensional Boundary Layers: B- Axisymmetric Boundary Layers
 
7 Three-Dimensional Boundary Layers: C- 3-D Boundary Layers
 
8 Three-Dimensional Boundary Layers: D- 3-D Boundary Layer Separation
 
9 Mid-term exam
 
10 Compressible Boundary Layers: A- Compressible Couette Flow B- Boundary Layer Equations
 
11 Compressible Boundary Layers: C- Transformations D- Flat Plate Boundary Layer
 
12 Compressible Boundary Layers: E- Boundary Layers with Pressure Gradient F- Boundary Layers with Suction G- Shock- Boundary Layer Interaction
 
13 Hypersonic Boundary Layers: A- Introduction B- Boundary Layer Equations
 
14 Hypersonic Boundary Layers: C- Flat Plate Boundary Layer