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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Main Author: Ainul, Azmel
Published: University of Manchester 2008
Subjects:
Online Access:http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494600
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spelling 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
collection NDLTD
sources NDLTD
topic 629.13432
spellingShingle 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
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