MDM512 VICOUS FLOW

Course Code:8760512
METU Credit (Theoretical-Laboratory hours/week):3 (3.00 - 0.00)
ECTS Credit:8.0
Department:Mechanical Design and Manufacturing
Language of Instruction:English
Level of Study:Graduate
Course Coordinator:
Offered Semester:Fall and Spring Semesters.

Course Objectives

At the end of this course, the student will understand the techniques for the solution of Navier-Stokes equations.

At the end of this course, the student will understand the principles of creeping flow.

At the end of this course, the student will understand the boundary layer theory.

At the end of this course, the student will understand the techniques for similar solutions of Navier-Stokes equations.

At the end of this course, the student will understand the techniques for eaxact solution of 2D boundary layer equations. 

At the end of this course, the student will understand the principles for the approximate solution of boundary layer equations.


Course Content

Outline of fluid motion with friction and boundary layer concept.Derivation of the equations of motion of a compressible viscous fluid(Navier-Stokes equations).General properties of Navier-Stokes equations,exact solutions of Navier-Stakes equations,creeping flow.Derivations of boundary layer equations,general properties of the boundary layer equations,exact solutions of the steady state boundary layer equations,approximate methods for the solution of the boundary layer flows.Boundary layer control.Stability of laminar flows.Transition.Fundamentals of turbulent flow.


Course Learning Outcomes

Ability to derive governing flow equations.

Ability to obtain exact solution of the Navier-Stokes equations for simple geometries.  the wave propagation phenomenon in subsonic, sonic and supersonic flows.

Ability to analyze creeping flows.

Ability to understand the basic principles behind the boundary layer theory.  

Ability to obtain similar solutions of boundary layer equations.

Ability to obtain exact solutions of 2D boundary layer equations.

Ability to obtain approximate solutions of 2D boundary layer equations.