4D5, 2022: Foundation engineering
Last updated on 20/01/2023 09:07
Last updated on 20/01/2023 09:07
Last updated on 20/01/2023 08:59
Last updated on 20/01/2023 08:55
Last updated on 20/01/2023 08:35
Fridays 11-1pm and Tuesdays 9-11am plus afternoons
2P6, 3F1 (desirable), 3G1 (desirable)
The aims of the course are to:
As specific objectives, by the end of the course students should be able to:
Please refer to Form & conduct of the examinations.
Last modified: 01/12/2025 07:27
Thursdays 11-1pm and Mondays 9-11am plus afternoons
2P6, 3F1 (desirable), 3G1 (desirable)
The aims of the course are to:
As specific objectives, by the end of the course students should be able to:
Please refer to Form & conduct of the examinations.
Last modified: 29/11/2024 15:21
Thursdays 11-1pm and Mondays 9-11am plus afternoons
2P6, 3F1 (desirable), 3G1 (desirable)
The aims of the course are to:
As specific objectives, by the end of the course students should be able to:
Please refer to Form & conduct of the examinations.
Last modified: 22/11/2022 20:15
Thursdays 11-1pm and Mondays 9-11am plus afternoons
3C6 useful
The aims of the course are to:
The intense vibration of a rocket launch poses significant challenges for the designers of any launch vehicle or its payload. This project considers the design of a vibration isolation system for a sensitive payload – a satellite containing a sensitive instrument. It involves modelling the vibration behaviour of a prototype satellite structure, the design and assembly of the isolation system, and some shaker testing to verify the final design. The work is based on theory and techniques introduced in Part IA Mechanical Vibrations and the Part IIA Module, 3C6.
FORMAT
Students work individually in Weeks 1 and 2, for which individual interim reports are submitted. The design exercise in Weeks 3 and 4 is undertaken in groups of three, in which each student is responsible for a specific design concept and the corresponding section of the final report.
Familiarisation with the prototype structure and test rig. Conduct initial vibration tests. Manual calculation of natural frequencies. First interim report.
Develop theoretical model. Predict vibration response and compare with initial test data. Update model. Second interim report.
Develop model to select and refine isolation design. Assemble prototype. Conduct shaker test to verify design. Final report and group presentation.
|
Interim Report 1 (individual) |
TBA |
15 |
|
Interim Report 2 (individual) |
TBA |
25 |
|
Final Report (group)
|
TBA |
40 (20:20 individual:group) |
Please refer to Form & conduct of the examinations.
Last modified: 29/11/2024 15:15
Thursdays 11-1pm and Mondays 9-11am plus afternoons
3C6 useful
The aims of the course are to:
The intense vibration of a rocket launch poses significant challenges for the designers of any launch vehicle or its payload. This project considers the design of a vibration isolation system for a sensitive payload – a satellite containing a sensitive instrument. It involves modelling the vibration behaviour of a prototype satellite structure, the design and assembly of the isolation system, and some shaker testing to verify the final design. The work is based on theory and techniques introduced in Part IA Mechanical Vibrations and the Part IIA Module, 3C6.
FORMAT
Students work individually in Weeks 1 and 2, for which individual interim reports are submitted. The design exercise in Weeks 3 and 4 is undertaken in groups of three, in which each student is responsible for a specific design concept and the corresponding section of the final report.
Familiarisation with the prototype structure and test rig. Conduct initial vibration tests. Manual calculation of natural frequencies. First interim report.
Develop theoretical model. Predict vibration response and compare with initial test data. Update model. Second interim report.
Develop model to select and refine isolation design. Assemble prototype. Conduct shaker test to verify design. Final report and group presentation.
|
Interim Report 1 (individual) |
TBA |
15 |
|
Interim Report 2 (individual) |
TBA |
25 |
|
Final Report (group)
|
TBA |
40 (20:20 individual:group) |
Please refer to Form & conduct of the examinations.
Last modified: 27/11/2023 09:46
Thursdays 11-1pm and Mondays 9-11am plus afternoons
3C6 useful
The aims of the course are to:
The intense vibration of a rocket launch poses significant challenges for the designers of any launch vehicle or its payload. This project considers the design of a vibration isolation system for a sensitive payload – a satellite containing a sensitive instrument. It involves modelling the vibration behaviour of a prototype satellite structure, the design and assembly of the isolation system, and some shaker testing to verify the final design. The work is based on theory and techniques introduced in Part IA Mechanical Vibrations and the Part IIA Module, 3C6.
FORMAT
Students work individually in Weeks 1 and 2, for which individual interim reports are submitted. The design exercise in Weeks 3 and 4 is undertaken in groups of three, in which each student is responsible for a specific design concept and the corresponding section of the final report.
Familiarisation with the prototype structure and test rig. Conduct initial vibration tests. Manual calculation of natural frequencies. First interim report.
Develop theoretical model. Predict vibration response and compare with initial test data. Update model. Second interim report.
Develop model to select and refine isolation design. Assemble prototype. Conduct shaker test to verify design. Final report and group presentation.
|
Interim Report 1 (individual) |
TBA |
15 |
|
Interim Report 2 (individual) |
TBA |
25 |
|
Final Report (group)
|
TBA |
40 (20:20 individual:group) |
Please refer to Form & conduct of the examinations.
Last modified: 28/11/2022 10:53