Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing
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 m...
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ndltd-bl.uk-oai-ethos.bl.uk-4946002015-03-20T05:16:55ZStructural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wingAinul, Azmel2008Classical 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.629.13432University of Manchesterhttp://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494600Electronic Thesis or Dissertation |
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629.13432 |
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629.13432 Ainul, Azmel Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
description |
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. |
author |
Ainul, Azmel |
author_facet |
Ainul, Azmel |
author_sort |
Ainul, Azmel |
title |
Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
title_short |
Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
title_full |
Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
title_fullStr |
Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
title_full_unstemmed |
Structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
title_sort |
structural and aeroelastic multidisciplinary optimisation of a joined-type sensorcraft wing |
publisher |
University of Manchester |
publishDate |
2008 |
url |
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494600 |
work_keys_str_mv |
AT ainulazmel structuralandaeroelasticmultidisciplinaryoptimisationofajoinedtypesensorcraftwing |
_version_ |
1716790293677735936 |