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Structural components of an aircraft. Loads on aircraft. Aircraft structural components and structural idealization. Open and closed thin walled tubes. Multicell structures. Axial constraint. Practical aircraft structural analysis. Buckling phenomenon. Buckling of columns and beam-columns.
| AUs | 3.0 AUs |
| Grade Type | |
| Prerequisite | MA2001 |
| Exam | 30 November 2026, 1.00 pm - 3.30 pm |
The Exam information shown may be subject to changes. Students are to check the finalised exam timetable with exam seat information, which will be available at the 'Examination Seating Arrangement' webpage, 2 weeks before start of examination.
Required first
MA2001Mechanics Of MaterialsAircraft Structures I
| Mon | Tue | Wed | Thu | Fri | |
|---|---|---|---|---|---|
| 930 | |||||
| 1000 | |||||
| 1030 | |||||
| 1100 | |||||
| 1130 | |||||
| 1200 | |||||
| 1230 | |||||
| 1300 | |||||
| 1330 | |||||
| 1400 | |||||
| 1430 | |||||
| 1500 | |||||
| 1530 | |||||
| 1600 | |||||
| 1630 | |||||
| 1700 | |||||
| 1730 | |||||
| 1800 |
| Mon | Tue | Wed | Thu | Fri | |
|---|---|---|---|---|---|
| 1430 | COMMON LEC (LE) 1430-1620 Mon LT8 | ||||
| 1500 | |||||
| 1530 | COMMON LEC (LE) 1530-1620 Wed LT9 | ||||
| 1600 |
