Aerospace Aerodynamics
| Code | School | Level | Credits | Semesters |
| MMME3080 | Mechanical, Materials & Manufacturing Engineering | 3 | 20 | Autumn UK |
- Code
- MMME3080
- School
- Mechanical, Materials & Manufacturing Engineering
- Level
- 3
- Credits
- 20
- Semesters
- Autumn UK
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
Students on one of the Aerospace Engineering courses H402, H40A, H400, H40B. Not available to any other students
Assessment
- 25% Coursework 1: LO3
- 25% Coursework 2: LO4
- 50% Exam 1 (2-hour): LO1, LO2
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 choice of aerodynamic components and their performance.Learning Outcomes
On successful completion of this module students will be able to:
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