AEROENG 5775
Transcript Abbreviation:
Hypersonic Flow
Course Description:
Introduction to hypersonic inviscid and viscous flows, Newtonian theory, high-temperature effects and heat transfer.
Course Levels:
Undergraduate (1000-5000 level)
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)
12 weeks (summer only)
Off Campus:
Never
Campus Location:
Columbus
Instruction Modes:
In Person (75-100% campus; 0-24% online)
Prerequisites and Co-requisites:
Prereq: 3570, or Grad standing in AeroEng.
Electronically Enforced:
No
Exclusions:
(N/A)
Course Goals / Objectives:
Students should understand principal features of hypersonic flows and how they differ from supersonic flow, classical hypersonics theories and their strengths and limitations
Continuum and non-continuum phenomena, High-Temperature effects, Reentry physics, Principal outstanding problems in hypersonics
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC | LAB | LAB Inst |
|---|---|---|---|---|
| Unique features of hypersonic flows | 5.0 | 0.0 | 0.0 | 0 |
| Classical theories | 6.0 | 0.0 | 0.0 | 0 |
| Viscous-inviscid interactions in hypersonic flows | 6.0 | 0.0 | 0.0 | 0 |
| Hypersonic transition and turbulence | 6.0 | 0.0 | 0.0 | 0 |
| Statistical thermodynamics and concept of non-equilibrium | 8.0 | 0.0 | 0.0 | 0 |
| High-Temperature effects: thermo-chemical nonequilibrium | 6.0 | 0.0 | 0.0 | 0 |
| Reentry physics, including radiation, ablation, ionization | 6.0 | 0.0 | 0.0 | 0 |
| Modern topics a. Electromagnetic flow control b. Scramjet propulsion c. Gas surface interactions | 6.0 | 0.0 | 0.0 | 0 |
| Total | 49 | 0 | 0 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Grade Roster Component:
Lecture
Credit by Exam (EM):
No
Grades Breakdown:
| Aspect | Percent |
|---|---|
| Homework | 10% |
| Quizzes(3) | 20% |
| Mid-term | 30% |
| Final | 40% |
Representative Textbooks and Other Course Materials:
| Title | Author | Year |
|---|---|---|
| Hypersonic and High Temperature Gas Dynamics | John D. Anderson Jr. |
ABET-CAC Criterion 3 Outcomes:
(N/A)
ABET-ETAC Criterion 3 Outcomes:
(N/A)
ABET-EAC Criterion 3 Outcomes:
| Outcome | Contribution | Description |
|---|---|---|
| 1 | Significant contribution (7+ hours) | an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics |
| 2 | Substantial contribution (3-6 hours) | an ability to apply engineering design to produce solutions that meet specified needs with consideration of public health, safety, and welfare, as well as global, cultural, social, environmental, and economic factors |
Embedded Literacies Info:
Attachments:
(N/A)
Additional Notes or Comments:
(N/A)
Basic Course Overview:
AEROENG_5775_basic.pdf
(9.61 KB)