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Title: Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing
Author: Ainul, Azmel
ISNI:       0000 0001 3403 3319
Awarding Body: University of Manchester
Current Institution: University of Manchester
Date of Award: 2008
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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.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID:  DOI: Not available