NG1S420 - Aerospace Mechanics 01 Aug 2023 - 31 Aug 2030 | Version 4
Associated Module Information
| Module Code: | NG1S420 | ||
|---|---|---|---|
| Module Title: | Aerospace Mechanics | ||
| Faculty: | Faculty of Computing, Engineering and Science | ||
| Faculty Group: | Aircraft Maintenance Engineering | ||
| Faculty Sub Group: | Aircraft Maintenance Engineering | ||
| Module Leader: | Pravin Krishnan | ||
| Module Team: | Alun Griffiths, Gary Dornan, Emily Simba, Michael Bates, Adrian Pitman, Shahrizam Ismail, Daniel Jones, Jason Blackwell | ||
| First Intended Intake: | SEP 2017 | Final Year of Intake: | 2028 |
| Date Closed: | |||
| Credit Value: | 20 | Credit Level: | 4 |
| Language: | English | ||
| Percentage of Module Taught in Welsh: | 0 | ||
| Equivalent Module: | |||
| HECOS codes: | 100430 - mechanics | ||
| HECOS Code Weighting: | 100 | ||
Document Version Information
| Version | 4 |
|---|---|
| Valid From | 01 Aug 2023 |
| Valid To | 31 Aug 2030 |
Module Aims
This module provides detailed theoretical knowledge and present practical task opportunities to further enhance student understanding of Aerodynamics, Aircraft Systems and Structures. Demonstrate an understanding of principles and applications of physics to airframe, propulsion technology as well as the aircraft engineering field.
Provides student with an understanding of the fundamental of physics.
Content Summary
Matter, Chemical elements, Changes between states
Mechanics,
Statics, Theory of stress, strain and elasticity
Kinetics, Linear movement, rotational movement, Periodic motion, Dynamics
Mass,, force, inertia, momentum, friction, Fluid Dynamics
Thermodynamics, heat definition, heat capacity, specific heat, 1st and 2nd Law of thermodynamics
Optics (Light)
Wave Motion and Sound
Flight stability and dynamics. Axis of rotation. Control & Stability
Aerodynamics and the Theory of Flight using correct terminology
Learning and Teaching Methods
| Activity Type | Hours |
|---|---|
| Lecture | 86 |
| Tutorial | 20 |
| Demonstration | 10 |
| Independent Study | 68 |
| Formative Assessment - Scheduled | 10 |
| Problem / challenge based learning | 6 |
| Total Hours Selected | 200 |
Learning Outcomes
| # | Learning Outcome |
|---|---|
| LO1 | Demonstrate an understanding of basic aerodynamics, flight stability and aircraft dynamics |
| LO2 | Demonstrate an understanding of principles and applications of physics to airframe and propulsion technology |
Module Requisites
N/A
Assessment Criteria
| Assessment Category | Assessment Type | Description | Duration | Word Count | Weight (%) | Best of? | Pass Mark |
|---|---|---|---|---|---|---|---|
| Synchronous Onsite Assessment (Exam) | Onsite External Examination 1 | 2 x Onsite External Examination - Part 66 Examination | 90 | N/A | 60 | No | 40 |
| Synchronous Onsite Assessment | Classroom Test - Time Constrained (Onsite) 1 | 1 x Class test | 60 | N/A | 40 | No | 40 |
Assessment Matrix
| Assessment Type | Learning Outcomes | ||
|---|---|---|---|
| LO1 | LO2 | ||
| Onsite External Examination 1 | ✔ | ✔ | |
| Classroom Test - Time Constrained (Onsite) 1 | ✔ | ✔ | |