Advanced Aerodynamics
| Code | School | Level | Credits | Semesters |
| AERO3007 | School of Aerospace | 3 | 20 | Autumn China |
- Code
- AERO3007
- School
- School of Aerospace
- Level
- 3
- Credits
- 20
- Semesters
- Autumn China
Summary
This module extends and deepens knowledge of students on the Aerospace Engineering courses in
aerodynamics in an aerospace context. It covers the following indicative content:
• Compressible flow and applications (e.g. supersonic aerofoils, nozzles and inlets)
• Shock wave theory
• Wing theories for low- and high-speed applications
• Transonic and supersonic flow
• Low- and high-speed flow control and drag reduction
Target Students
Target Students: Students on one of the Aerospace Engineering courses H402, H40A, H400, H40B. Not available to any other students including exchange students.
Classes
- Two 2-hour lectures each week for 12 weeks
Assessment
- 25% Coursework 1
- 25% Coursework 2
- 50% Exam 1 (2-hour)
Assessed by end of autumn semester
Educational Aims
The aim of this module is for students to understand classical flows relevant to the low- and high-speed aerodynamic design of aircraft. Students should be able to make decisions based on knowledge and calculations with regards to choose of aerodynamic components and their performance.Learning Outcomes
LO1 - Comprehend and apply knowledge of the fundamentals of compressible flow and wing
theories for low and high flight speeds
LO2 - Demonstrate understanding of the major aerodynamic design challenges and drag reduction
technologies and strategies used in aerospace applications for different flight regimes
LO3 - Develop an analytical and/or numerical methodology to conduct an aerodynamics investigation
of an aerospace configuration and communicate its implications
LO4 - Record and evaluate the salient details from an experimental and/or computational
investigation and conduct accurate and appropriate data analysis
Conveners
- Dr Richard Adjei