Use the Tab and Up, Down arrow keys to select menu items.
This course covers more in-depth engineering design methods than ENME301 and covers procedures that are not included in the engineering science subjects. The subject matter will have an aerospace design focus and will include additional content to cover aerospace conceptual design, cost and weight estimation, configuration and layout, basic aircraft performance; aircraft subsystems; lifecycle topics; safety and reliability certification requirements, risk analysis and management. Overall students are brought to a level where they can undertake a substantial aerospace engineering design problem in a methodical manner, and can produce a professional quality design report.
This course is an elective for Mechanical Engineering students who are attempting the Aerospace Minor.
Washington Accord (V4) Summary of Graduate Attributes attained in this course: WA1 – Engineering Knowledge WA2 – Problem Analysis WA3 – Design/Development of Solutions WA5 – Tool Usage WA6 – The Engineer and the World WA7 – Ethics WA10 – Project Management and FinanceCourse topics with Learning Outcomes (and Washington Accord (WA) and UC Graduate Attributes) identified.1. Aerospace conceptual design and step-by-step design development 1.1. Ability to perform conceptual design of different types of aircraft (WA1, WA3, WA10) (EIE2, EIE3)Range: Overview of the design process; sizing from a conceptual sketch; engineering drawings, dimensioning, and tolerancing 1.2. Understand the method of preparation of design tasks and technical reports (WA3, WA5, WA10) (EIE2)2. Cost and weight estimation, and configuration and layout 2.1. Able to calculate total weight and weight features of an aircraft, and perform and understand sizing of an aircraft (WA1, WA2, WA3, WA5) (EIE3)Range: Airfoil and wing/tail geometry selection; thrust-to-weight ratio and wing loading; initial sizing; configuration layout and loft; special considerations in configuration layout; crew station, passengers, and payload 3. Basic aircraft performance and aircraft subsystems 3.1. Able to calculate performance characteristics of an aircraft (WA1, WA2, WA11)Range: propulsion and fuel system integration; landing gear and subsystems; step-by-step development of a new design; aerodynamics; propulsion; structures and loads; weights; stability, control, and handling qualities; performance and flight mechanics; cost analysis; sizing and trade-off studies; fatigue design; joining4. Lifecycle topics, e.g. environmental issues (pollution, energy, etc.); safety and reliability certification requirements, and risk analysis, ethics and management 4.1. Understand design responsibilities regarding risk, reserve/safety factors, environmental, and ethical considerations (WA6, WA7, WA8) (EIE3)Range: risk assessment, certification, regulatory bodies and use of standards; lifecycle, environmental and ethical issues
This course will provide students with an opportunity to develop the Graduate Attributes specified below:
Employable, innovative and enterprising
Students will develop key skills and attributes sought by employers that can be used in a range of applications.
ENME201, ENME221, ENME301
ENME311, ENME351
Students must attend one activity from each section.
Stephen Daynes
https://www.canterbury.ac.nz/study/academic-study/engineering/schools-and-departments-engineering-forestry-product-design/mechanical-engineering-department/minor-in-aerospace-engineering
For detailed course, policy, regulatory and integrity information, please refer to the UC web site, or see relevant Course or Department LEARN pages, (which are available to enrolled students).
• This course has a capacity of 40 students. Selection criteria is on 2nd Yr GPA, and at the discretion of the Department. Students must declare the Minor and enrol in this course, by day 1 of Term 1 of 3rd Yr, to be considered.
Domestic fee $1,059.00
International fee $6,000.00
* All fees are inclusive of NZ GST or any equivalent overseas tax, and do not include any programme level discount or additional course-related expenses.
Maximum enrolment is 41
For further information see Mechanical Engineering .