Course Information
SemesterCourse Unit CodeCourse Unit TitleT+P+LCreditNumber of ECTS Credits
5MAK356Fluid Mechanics I3+0+035

Course Details
Language of Instruction Turkish
Level of Course Unit Bachelor's Degree
Department / Program Mechanical Engineering
Mode of Delivery Face to Face
Type of Course Unit Compulsory
Objectives of the Course 1 - Learn ALL of the fundamentals of subsonic and supersonic ideal compressible fluid flows.
2 - Learn fundamentals of isentropic flows in Laval and other nozzles.
3 - Learn the solution of the problems of NorMAL and reflected shock waves.
4 - Mastering solutions of frictional or not or adiabatik or not compressible flows in LonG or short and insulated or not pipes.
5 - Obtain a general understanding of the principles of two-dimensional supersonic flows.
Course Content Fundamentals of fluid mechanics and thermodynamics. Introduction to compressible flows. Isentropic flow. Normal shock waves; moving and reflected shock waves. Flow in constant area ducts with friction; Fanno line, choking due to friction. Flow in constant area ducts with heat transfer; Rayleigh line, choking due to heat transfer. Isothermal frictional flow in uninsulated ducts, Steady two dimensional supersonic flows; oblique shock waves, Prandtl Meyer flow.
Course Methods and Techniques
Prerequisites and co-requisities None
Course Coordinator None
Name of Lecturers Prof.Dr. Mehmet Ali Baykal
Assistants None
Work Placement(s) No

Recommended or Required Reading
Resources Compressible Fluid Flow, P.H. Oosthuizen and W. E. Carscallen McGraw-Hill, 1997.
Compressible Fluid Dynamics with PC Applications, B. K. Hodge and K. Koenig, Prentice Hall, 1995.
Modern Compressible Flow, J. D. Anderson, McGraw-Hill, 1990.
Gas Dynamics, M. J. Zucrow and J. D. Hoffman, John Willey & Sons, Inc., 1977.
Lecture
1 Ara sınav, 1 Final sınavı


Planned Learning Activities and Teaching Methods
Activities are given in detail in the section of "Assessment Methods and Criteria" and "Workload Calculation"

Assessment Methods and Criteria
In-Term Studies Quantity Percentage
Mid-terms 1 % 16
Quizzes 3 % 24
Final examination 1 % 60
Total
5
% 100

 
ECTS Allocated Based on Student Workload
Veri yok

Course Learning Outcomes: Upon the successful completion of this course, students will be able to:
NoLearning Outcomes
1 Formulate and solve problems in one dimensional steady compressible flows.
2 Solve the problems of steady isentropic flow of ideal gases in Laval nozzles.
3 Calculate the change in pressure, density and temperature for flows through normal and reflected shock waves.
4 Solve the problems of adiabatic frictional (Fanno) flows in long constant area ducts.
5 Solve the problems of frictional , uninsulated (Isothermal) constant area duct flows.
6 Solve the problems of frictionless flows with heat transfer (Rayleigh) in short ducts.
7 Solve oblique shock wave problems of supersonic flows around wedge shaped bodies and concave corners.
8 Determine the change in flow conditions through a Prandtl Meyer expansion wave.


Weekly Detailed Course Contents
WeekTopicsStudy MaterialsMaterials
1 Review of thermodynamics
2 Governing equations of fluid dynamics and energy
3 One-dimensional compressible flow
4 Isentropic flow, normal shock relations
5 Fanno and Rayleigh lines, Rankine-Hugoniot relation
6 Convergent-divergent nozzles
7 Isentropic flow in ducts
8 Isentropic flow in ducts
9 FINAL EXAM
10 Shock waves
11 Shock waves
12 Blast waves, shock tubes
13 Mach lines
14 Prandtl-Meyer function
15 The Method of Characteristics
16 FINAL EXAM


Contribution of Learning Outcomes to Programme Outcomes
P1 P2 P3 P4 P5 P6 P7 P8 P9 P10 P11
C1 5
C2 5
C3 5
C4 5
C5 5
C6 5
C7 5
C8 5

bbb


https://obs.gedik.edu.tr/oibs/bologna/progCourseDetails.aspx?curCourse=205722&curProgID=73&lang=en