Module Details
Module Code: |
DSGN H4602 |
Module Title:
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Conceptual Design
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Title:
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Conceptual Design
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Module Level:: |
8 |
Module Coordinator: |
Cathal Nolan
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Module Author:: |
Edmond Tobin
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Module Description: |
The aim of the module is to provide learners with the techniques and knowledge required to perform a conceptual design of a light aircraft. Conceptual design techniques will be presented on aerodynamics, structures, performance, and propulsion systems. Students have to work together in a virtual industrial environment and carry out individual tasks upon which the whole team is dependent.
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Learning Outcomes |
On successful completion of this module the learner will be able to: |
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Learning Outcome Description |
LO1 |
Apply conceptual design techniques to develop a series of conceptual designs and iterate to a design solution based on a specification. |
LO2 |
Work effectively as a team member in the planning, managing, organising and completion of tasks among a group of peers. |
LO3 |
Assess ethical issues in relation to group work and sustainability of the final design. |
LO4 |
Evaluate aircraft designs using software applications and numerical analysis. |
LO5 |
Resolve conflicting issues within a team dynamic, in both leadership and specialist positions. |
Dependencies |
Module Recommendations
This is prior learning (or a practical skill) that is recommended before enrolment in this module.
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No recommendations listed |
Co-requisite Modules
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No Co-requisite modules listed |
Additional Requisite Information
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No Co Requisites listed
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Indicative Content |
Design Process
- Introduction
- Phases of Aircraft Design
- Conceptual Design Process
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Initial Sizing
- Takeoff Weight
- Empty Weight and Fuel Fraction
- Powerplant Sizing
- Geometry Sizing
- Control Surface Sizing
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Conceptual Layout
- Vertical Wing Location
- Wing Configuration, Dihedral, Structural
- Cabin Configuration
- Propeller Configuration
- Empennage Configuration
- Landing Gear Configuration
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Weights Analysis
- Initial Weight Analysis Methods
- Detailed Weight Analysis Methods
- Statistical Weight Analysis Methods
- Direct Weight Analysis Methods
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Cost Analysis
- Elements of Life-Cycle Cost
- Sustainability, End of Life Considerations
- Production, Operation and Maintenance Costs
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Performance and Aerodynamics
- Aerofoil Geometries
- Forces and Moments
- High Lift Devices
- Wingtip Design
- Take-off
- Climb
- Cruise
- Range Analysis
- Descent
- Landing
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Project Brief
Initially, the team will be presented with a conceptual design and a budget. The team will have to produce a:
- Design Specification
- Objectives
- Literature search
- Project management plan
- Address any ethical issues in relation to the design
- Assess the sustainability of the design.
The supervisor will discuss the assessment plan with the team to ensure a clear understanding
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Team structure
Team members will be assigned responsibilities for the following key areas:
Team leader ( rotating position between team members)
Propulsion system
Aerodynamics
Control system
Software / Hardware design
System Integration
Testing
Quality control / budget costs
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Presentation
The student will be required to make presentations on the progress of their project. A final presentation by the team or member on the completed design
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Thesis
Formal report on the final project
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Module Content & Assessment
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Assessment Breakdown | % |
Continuous Assessment | 60.00% |
Project | 40.00% |
AssessmentsFull Time
No End of Module Formal Examination |
Reassessment Requirement |
Repeat examination
Reassessment of this module will consist of a repeat examination. It is possible that there will also be a requirement to be reassessed in a coursework element.
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SETU Carlow Campus reserves the right to alter the nature and timings of assessment
Module Workload
Workload: Full Time |
Workload Type |
Workload Category |
Contact Type |
Workload Description |
Frequency |
Average Weekly Learner Workload |
Hours |
Lecture |
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Contact |
Design techniques and aircraft case studies |
12 Weeks per Stage |
2.00 |
24 |
Laboratory |
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Contact |
Software labs and group work |
12 Weeks per Stage |
2.00 |
24 |
Independent Learning Time |
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Non Contact |
No Description |
15 Weeks per Stage |
5.13 |
77 |
Total Weekly Contact Hours |
4.00 |
Module Resources
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Recommended Book Resources |
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Daniel P. Raymer. (2018), Aircraft Design, 6th. Amer Inst of Aeronautics & Astronautics, p.1062, [ISBN: 1624104908].
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Snorri Gudmundsson. (2013), General Aviation Aircraft Design, Butterworth-Heinemann, p.1048, [ISBN: 9780123973290].
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Nigel J. Smith. Engineering Project Management, Wiley-Blackwell, p.400, [ISBN: 1405168021].
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Charles E. Harris, Jr.,Michael S. Pritchard,Michael J. Rabins,Ray James,Elaine Englehardt. (2018), Engineering Ethics: Concepts and Cases, 6th. Cengage Learning, p.336, [ISBN: 1337554502].
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Elizabeth Hoppe. (2018), Ethical Issues in Aviation, 2nd. Routledge, p.362, [ISBN: 1472470869].
| Supplementary Book Resources |
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James G. Speight,Russell Foote. (2011), Ethics in Science and Engineering, John Wiley & Sons, p.320, [ISBN: 047062602X].
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Thomas C. Corke. (2003), Design of Aircraft, 1st. Pearson College Division, p.391, [ISBN: 0130892343].
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Jan Roskam,Chuan-Tau Edward Lan. (1997), Airplane Aerodynamics and Performance, DARcorporation, p.711, [ISBN: 1884885446].
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Darrol Stinton. (2001), The Design of the Aeroplane, 2nd. Wiley-Blackwell, p.684, [ISBN: 0632054018].
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[compiled by] Deborah G. Johnson. (1991), Ethical issues in engineering, Prentice Hall, Englewood Cliffs, N.J., [ISBN: 0132905787].
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Charles Stephen Lessard. (2007), Project Management for Engineering Design, Morgan & Claypool Publishers, p.110, [ISBN: 1598291742].
| This module does not have any article/paper resources |
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Other Resources |
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On-line text book -
http://itll.colorado.edu/index.php/cours
es_workshops/geen_1400/resources/textboo
k.
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http://www.ldeo.columbia.edu/~martins/se
n_sem/thesis_org.html.
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HAW Hamburg. MOOC,
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EASA. EASA,
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OpenVSP,
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Aircraft Design Software,
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