Download 20-AEEM-641 - Department of Aerospace Engineering and

Survey
yes no Was this document useful for you?
   Thank you for your participation!

* Your assessment is very important for improving the workof artificial intelligence, which forms the content of this project

Document related concepts

Turbulence wikipedia , lookup

Derivation of the Navier–Stokes equations wikipedia , lookup

Reynolds number wikipedia , lookup

Aerodynamics wikipedia , lookup

Fluid dynamics wikipedia , lookup

Navier–Stokes equations wikipedia , lookup

Boundary layer wikipedia , lookup

Transcript
20-AEEM-641
Intro. to Compressible Flow
University of Cincinnati
Department of Aerospace Engineering
745 Baldwin Hall, ML 0070
Cincinnati, OH 45221
(513) 556-3553
Course Coordinator: S. Abdallah
Office Hours:
Date of Preparation: 7/29/2003
Prepared by: S. Abdallah
Revised:
Catalog Description
Boundary layer methods for two dimensional and axisymmetric incompressible steady flows. Current solution
methods. Introduction to turbulent flows. 3 gr. cr.
Reference
H. Schlichting, Boundary Layer Theory, 7th Ed., McGraw-Hill, 1979.
T. Cebeci and P. Bradshaw, Momentum Transfer in Boundary Layers,
McGraw-Hill, 1977.
Prerequisite
20-AEEM-342
Text
Course Objectives
The emphasis in this course is on the theoretical development of solution techniques for the
compressible and incompressible boundary layer equations. The boundary layer equations are derived in
general surface coordinates and details of exact and approximate methods of solution are presented.
Topics Covered
1. The Navier-Stokes compressible and incompressible equations. (6 hours)
2. Exact solutions to the laminar incompressible boundary layer equations. General similarity concepts.
Solutions to the Falkner-Skan equations. Forward and reverse flow. Finite difference methods. Blasius
series method. (8 hours)
3. Modern numerical algorithms for two-point boundary value problems. Applications to typical problems.
(6 hours)
4. Approximate solution of laminar compressible boundary layer equations. Local similarity. KarmanPohlhausen method. Compressibility transformation. (6 hours)
5. Introduction to turbulent boundary layers. Eddy viscosity concept. (2 hours)
6. Tests. (2 hours)
Contribution of Course to Meeting Professional Experience
Component Addressed by AEEM
Required Professional Component
641
a) Mathematics
b) Engineering
X
c) General Education
d) Design Experience
X
Instrument of Assessment
Course Name: Intro. To Compressible Flow
Quarter_______________________________
Outcome
Objective
HW
Course # AEEM-641
Instructor_____________________________
Quiz
MidTerm
Final
Report
a) An ability to apply knowledge
of mathematics, science, and
engineering to problems in the
aerospace disciplines
b) An ability to design and
conduct experiments, as well as to
analyze and interpret data
c) An ability to design an
aerospace system, component, or
process to meet desired needs
d) An ability to function on
multidisciplinary teams
e) An ability to identify,
formulate, and solve engineering
problems in the aerospace
disciplines
f) An understanding of
professional and ethical
responsibility
g) An ability to communicate
effectively in written and oral
presentation
h) The broad education
necessary to understand the impact
of engineering solutions in a global
and societal context
i) A recognition of the need for
an ability to engage in life-long
learning
j) A knowledge of contemporary
issues through participation in a
general education program
k) An ability to use the
techniques, skills, and modern
engineering tools necessary for
engineering practice
l) Enhanced understanding of
the relationship between theory
and professional practice through
the cooperative education
experience
m) The opportunity to specialize
and to participate in a research
experience
Notes:
1) Please attach a list of assignments, quizzes and exams.
2) Please add comments or concerns regarding the present assessment.
3) Please provide any comments or suggestions for improvement.
Oral
% of
Stud.
with C
and
above
Comments