Thermodynamics and Aerospace Propulsion
| Code | School | Level | Credits | Semesters |
| MMME2028 | Mechanical, Materials & Manufacturing Engineering | 2 | 20 | Full Year UK |
- Code
- MMME2028
- School
- Mechanical, Materials & Manufacturing Engineering
- Level
- 2
- Credits
- 20
- Semesters
- Full Year UK
Summary
This module will cover fundamental thermodynamics including key underlying equation sets such as the first and second law of thermodynamics, perfect gas relationships and analysis of relevant cycles for Aerospace propulsion such as the Brayton cycle. This content will be linked to the Aerospace Aerodynamics from MMME1030 to show how thermodynamics and aerodynamics are used jointly in the design of components and systems for aerospace propulsion. The principles of aircraft propulsion are further developed with a focus on jet engines including the principles of gas turbine engines, their layout and the application of compressible flow and turbomachinery principles. Factors influencing design and choice of engine configuration are introduced.
Re-assessment
Students who fail this module overall and are required to complete a re-assessment will be re-assessed by exam. The re-assessment exam mark alone will be used to determine whether students satisfy progression requirements.
Target Students
Students must be on one of the Aerospace Engineering courses H402, H40A, H400, H40B.
Assessment
- 20% Coursework 1: LO3
- 20% Coursework 2: LO4
- 60% Exam 1 (2-hour): Exam (LO1, LO2)
Assessed by end of spring semester
Educational Aims
The aim for this module is that students can assess an appropriate propulsion unit for a defined aircraft mission using their prior knowledge of aerodynamics combined with the material taught in this module.Learning Outcomes
On successful completion of this module students will be able to:
- L01 Comprehend relevant thermodynamics and be able to apply them in the analysis of propulsion units (AHEP 1)
- L02 Use their prior knowledge of aerodynamics to analyse blade systems relating to propulsion units (propeller, compressor/turbine blades) (AHEP 1)
- L03 Evaluate and appraise an aerospace system or powerplant system (AHEP 2)
- L04 Record the salient details from an experimental and/or computational investigation and conduct accurate and appropriate data analysis. (AHEP 2)