| Use this URL to cite or link to this record in EThOS: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494600 |
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| Title: | Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing | ||||
| Author: | Ainul, Azmel |
ISNI:
0000 0001 3403 3319
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| Awarding Body: | University of Manchester | ||||
| Current Institution: | University of Manchester | ||||
| Date of Award: | 2008 | ||||
| Availability of Full Text: |
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| Abstract: | |||||
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Classical criteria of aircraft design involve adding a multiplier to the structure's inertial load to cater for various flight circumstances. The value of this multiplier depends on the type of aircraft designed, for example a high value is used in acrobatic variants to cater for their high g manoeuvres, as compared to a lower value in light non-acrobatic versions.
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| Supervisor: | Not available | Sponsor: | Not available | ||
| Qualification Name: | Thesis (Ph.D.) | Qualification Level: | Doctoral | ||
| EThOS ID: | uk.bl.ethos.494600 | DOI: | Not available | ||
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