MECH ENG 4108 - Aircraft Design
North Terrace Campus - Semester 2 - 2016
The course information on this page is being finalised for 2016. Please check again before classes commence.
General Course Information
Course Code MECH ENG 4108 Course Aircraft Design Coordinating Unit School of Mechanical Engineering Term Semester 2 Level Undergraduate Location/s North Terrace Campus Units 3 Contact Up to 4.5 hours per week Available for Study Abroad and Exchange Y Incompatible MECH ENG 4062 Assumed Knowledge MECH ENG 3101, MECH ENG 3100 Course Description Aircraft design methodology, Technical task preparation, team working, Aircraft design organisation, Aircraft weight calculation, mission fuel weight, Sensitivity analysis, Standard requirements, First estimation of aircraft design parameters, Sizing, Drag polar estimation at low speed, Matching diagram, Aircraft three view and drawings, Overall configuration design, Fuselage design, Propulsion system selection and integration, Wing design considerations, Empennage design considerations, Landing gear design and integration, Weight and balance analysis, Stability and control analysis.
Course Coordinator: Dr Maziar Arjomandi
The full timetable of all activities for this course can be accessed from Course Planner.
Course Learning Outcomes
1 To equip students with the required knowledge to conduct conceptual design of different types of aircraft 2 To make the required decisions during the total design cycle of an aircraft including conceptual, preliminary and detail design 3 To provide understanding of analysis and assessment of different types of aircraft 4 To understand the hierarchical models in aircraft design as a multi-disciplinary design objective and utilise a system approach to design and operational performance 5 To distinguish and understand the design phases of an aircraft 6 To understand the method of preparation design tasks and technical reports 7 To be able to calculate total weight and weight fractures of an aircraft 8 To evaluate and understand sensitivity analysis of design parameters 9 To perform and understand sizing of an aircraft 10 To understand layout design of different aircraft 11 To be able to calculate performance characteristics of aircraft 12 To Understand the technology edges and the areas of research in Aerospace and Aeronautics 13 To appreciate environmental issues associated with the area of Aeronautics, such as energy conservation, pollution etc. 14 To develop problem solving skills i.e. identify main issues in aeronautical problems, simplify the problem and solve it using standard tools.
University Graduate Attributes
No information currently available.
Course notes – these are essential and required.
J. Roskam, Airplane Design I & II, 2nd Edition, 1989
Jan Roskam, Airplane Design , part III-VIII, 2002
John Anderson, Aircraft Performance and Design, 1999
Darrol Stinton, The Design of the Aeroplane, 2003
Daniel Raymer, Aircraft Design (a conceptual approach),1999
Learning & Teaching Activities
Learning & Teaching Modes
No information currently available.
The information below is provided as a guide to assist students in engaging appropriately with the course requirements.
As per university recommendations, it is expected that students spend 48hrs/week during teaching periods, and that a 3 unit course has a minimum workload of 156 hours regardless of the length of the course. Additional time may need to be spent acquiring assumed knowledge, working on assessment during non-teaching periods, and preparing for and attending examinations.
Learning Activities Summary
1. Introduction and Review – 5%1.1. Course organization and policies1.2. Review of “Aeronautical Engineering I” course1.3. Course and design project topics
2. Weight Estimation – 20%2.1. Weight equation2.2. Aircraft mission diagram2.3. Determination of payload weight
2.4. Determination of mission fuel weight
2.5. Empty weight estimation
3. Sensitivity studies – 10%3.1. Sensitivity of takeoff weight to payload weight3.2. Sensitivity of takeoff weight to empty weight3.3. Sensitivity of takeoff weight to performance parameters
4. Sizing – 30%4.1. Drag polar estimation4.2. Sizing to stall speed requirements4.3. Sizing to takeoff distance requirements
4.4. Sizing to landing distance requirements
4.5. Sizing to climb requirements
4.6. Sizing to manoeuvring requirements
4.7. Matching of all sizing requirements
5. Configuration Design – 35%5.1. Selection of the overall configuration5.2. Method of choosing overall configuration5.3. Design of cockpit and fuselage layout
5.4. Selection and integration of the propulsion system
5.5. Wing planform design
5.6. Empennage sizing
5.7. Control surface sizing
5.8. Landing gear sizing and disposition
5.9. Weight and balance analysis
Specific Course RequirementsNONE
The University's policy on Assessment for Coursework Programs is based on the following four principles:
- Assessment must encourage and reinforce learning.
- Assessment must enable robust and fair judgements about student performance.
- Assessment practices must be fair and equitable to students and give them the opportunity to demonstrate what they have learned.
- Assessment must maintain academic standards.
Assessment SummaryAll assessment tasks are summative. There are 2 assignments, together worth 10%, one laboratory report worth 10%, a group project worth 20%, and a combined open+closed book exam worth 60% of the total assessment. All assignments are due by 4pm on the due date. Details of each task are tabulated below.
Assessment task Weighting % Description Due date Learning objectives (see 2.1 above) Assignment 1 5 Weight calculation Ref to Lecture Notes 1-5 Assignment 2 5 Matching diagram Ref. to Lecture Notes 1-5 Laboratory report 10 Flight simulator laboratory Ref. to Lab Manual Design project 20 Group project Ref. to Lecture Notes 1-10 Final Exam 60 Exam on all parts of the course Exam period 1-10
Assessment Related RequirementsNONE
The solutions to the assignments will be reviewed and marked by the course tutor/s according to the marking rubric. The solutions will be available to the students on MyUni after the submission date. The group project will be marked based on 50% group mark and 50% individual contribution using a peer assessment method. The project assessment rubric is presented below:
Section/Criteria Mark (total 100) 1- External design /10 2- Weight calculation /5 3- Matching diagram /10 4- Configuration design /15 5- Drawings /20 6- Format and clarity /15 7- Research activities /10 8- Completeness /15
The hard copy of all assignments must be submitted in the labelled box on level 2 of Engineering South Building. Any assignments submitted as a hard copy must be accompanied by an assessment cover sheet available from room S116 or near the assignment submission area. Late assignments will be penalised 10% per day. Extensions for all assignments will only be given in exceptional circumstances and a case for this with supporting documentation can be made in writing after a lecture or via email to the lecturer who set the assignment. Hard copy assignments will be assessed and returned in 2 weeks of the due date. There will be no opportunities for re-submission of work of unacceptable standard. Due to the large size of the class feedback on assignments will be limited to in-class discussion resulting from questions from students.
Grades for your performance in this course will be awarded in accordance with the following scheme:
M10 (Coursework Mark Scheme) Grade Mark Description FNS Fail No Submission F 1-49 Fail P 50-64 Pass C 65-74 Credit D 75-84 Distinction HD 85-100 High Distinction CN Continuing NFE No Formal Examination RP Result Pending
Further details of the grades/results can be obtained from Examinations.
Grade Descriptors are available which provide a general guide to the standard of work that is expected at each grade level. More information at Assessment for Coursework Programs.
Final results for this course will be made available through Access Adelaide.
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