AEROENG 6560
Transcript Abbreviation:
Adv Aerodynamics
Course Description:
Advanced elements of aerodynamics across the entire Mach range.
Course Levels:
Graduate
Designation:
Elective
General Education Course
(N/A)
Cross-Listings
(N/A)
Credit Hours (Minimum if “Range”selected):
3.00
Max Credit Hours
(N/A)
Select if Repeatable:
Off
Maximum Repeatable Credits
(N/A)
Total Completions Allowed
(N/A)
Allow Multiple Enrollments in Term:
No
Course Length:
14 weeks (autumn or spring)
Off Campus:
Never
Campus Location:
Columbus
Instruction Modes:
In Person (75-100% campus; 0-24% online)
Prerequisites and Co-requisites:
Graduate standing in mechanical engineering or aerospace engineering or by permission of instructor.
Electronically Enforced:
Yes
Exclusions
(N/A)
Course Goals / Objectives:
Students will develop fundamental knowledge of aerodynamics across the entire Mach number range.
Students will understand and use fundamental tools for the analysis and design involved in aerodynamics across the entire Mach
number range.
number range.
Students will understand and develop advanced numerical analysis techniques involved in aerodynamics.
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC | LAB | LAB Inst |
|---|---|---|---|---|
| Review of linearized theory and similarity | 3 | 0 | 0 | 0 |
| Airfoil characteristics | 3 | 0 | 0 | 0 |
| Extreme flight conditions; high altitude, high angles-of-attack | 6 | 0 | 0 | 0 |
| Transonic drag rise and lift characteristics | 6 | 0 | 0 | 0 |
| Supersonic lift and drag characteristics; area ruling; slender-body theory | 6 | 0 | 0 | 0 |
| Hypersonic lift and drag characteristics, configurations | 6 | 0 | 0 | 0 |
| Numerical procedures in aerodynamics | 4 | 0 | 0 | 0 |
| Applications of computational fluid dynamics | 3 | 0 | 0 | 0 |
| Best practices in wind tunnel testing, data acquisition | 3 | 0 | 0 | 0 |
| Total | 40 | 0 | 0 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Grade Roster Component:
Lecture
Credit by Exam (EM):
No
Grades Breakdown:
| Aspect | Percent |
|---|---|
| Homework Assignments | 75% |
| Midterm Exam | 10% |
| Final Exam | 15% |
Representative Textbooks and Other Course Materials:
| Title | Author | Year |
|---|---|---|
| Aerodynamics for Engineers | J. J. Bertin | |
| Fluid-Dynamic Lift and (2) Fluid-Dynamic Drag | S. F. Hoerner |
ABET-CAC Criterion 3 Outcomes
(N/A)
ABET-ETAC Criterion 3 Outcomes
(N/A)
ABET-EAC Criterion 3 Outcomes
(N/A)
Embedded Literacies Info
(N/A)
Attachments
(N/A)
Additional Notes or Comments
(N/A)