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Rotational and ply-level uncertainty in response of composite shallow conical shells

S. Dey, T. Mukhopadhyay, H. Haddad Khodaparast, P. Kerfriden, S. Adhikari, Sondipon Adhikari Orcid Logo, Hamed Haddad Khodaparast Orcid Logo

Composite Structures, Volume: 131, Pages: 594 - 605

Swansea University Authors: Sondipon Adhikari Orcid Logo, Hamed Haddad Khodaparast Orcid Logo

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DOI (Published version): 10.1016/j.compstruct.2015.06.011

Abstract

This paper presents the quantification of rotational and ply level uncertainty of random natural frequency for laminated composite conical shells by using surrogate modeling approach. The stochastic eigenvalue problem is solved by using QR iteration algorithm. Sensitivity analysis is carried out to...

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Published in: Composite Structures
ISSN: 0263-8223
Published: 2015
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URI: https://cronfa.swan.ac.uk/Record/cronfa22148
first_indexed 2015-06-24T02:07:09Z
last_indexed 2019-04-02T09:29:55Z
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spelling 2019-03-31T17:32:14.4658289 v2 22148 2015-06-23 Rotational and ply-level uncertainty in response of composite shallow conical shells 4ea84d67c4e414f5ccbd7593a40f04d3 0000-0003-4181-3457 Sondipon Adhikari Sondipon Adhikari true false f207b17edda9c4c3ea074cbb7555efc1 0000-0002-3721-4980 Hamed Haddad Khodaparast Hamed Haddad Khodaparast true false 2015-06-23 ACEM This paper presents the quantification of rotational and ply level uncertainty of random natural frequency for laminated composite conical shells by using surrogate modeling approach. The stochastic eigenvalue problem is solved by using QR iteration algorithm. Sensitivity analysis is carried out to address the influence of different input parameters on the output natural frequencies. The sampling size and computational cost is reduced by employing the present approach compared to direct Monte Carlo simulation. The stochastic mode shapes are also depicted for a typical laminate configuration. Statistical analysis is presented to illustrate the results and its performance. Journal Article Composite Structures 131 594 605 0263-8223 Rotational uncertainty, Central composite design method, Natural frequency, Shallow conical shell, Sensitivity analysis, Stochastic mode shapes 1 11 2015 2015-11-01 10.1016/j.compstruct.2015.06.011 COLLEGE NANME Aerospace, Civil, Electrical, and Mechanical Engineering COLLEGE CODE ACEM Swansea University 2019-03-31T17:32:14.4658289 2015-06-23T17:20:47.5141987 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised S. Dey 1 T. Mukhopadhyay 2 H. Haddad Khodaparast 3 P. Kerfriden 4 S. Adhikari 5 Sondipon Adhikari 0000-0003-4181-3457 6 Hamed Haddad Khodaparast 0000-0002-3721-4980 7 0022148-11022016140321.pdf HaddadAndhikari2015Postprintv2.pdf 2016-02-11T14:03:21.6970000 Output 2109420 application/pdf Accepted Manuscript true 2016-06-11T00:00:00.0000000 true
title Rotational and ply-level uncertainty in response of composite shallow conical shells
spellingShingle Rotational and ply-level uncertainty in response of composite shallow conical shells
Sondipon Adhikari
Hamed Haddad Khodaparast
title_short Rotational and ply-level uncertainty in response of composite shallow conical shells
title_full Rotational and ply-level uncertainty in response of composite shallow conical shells
title_fullStr Rotational and ply-level uncertainty in response of composite shallow conical shells
title_full_unstemmed Rotational and ply-level uncertainty in response of composite shallow conical shells
title_sort Rotational and ply-level uncertainty in response of composite shallow conical shells
author_id_str_mv 4ea84d67c4e414f5ccbd7593a40f04d3
f207b17edda9c4c3ea074cbb7555efc1
author_id_fullname_str_mv 4ea84d67c4e414f5ccbd7593a40f04d3_***_Sondipon Adhikari
f207b17edda9c4c3ea074cbb7555efc1_***_Hamed Haddad Khodaparast
author Sondipon Adhikari
Hamed Haddad Khodaparast
author2 S. Dey
T. Mukhopadhyay
H. Haddad Khodaparast
P. Kerfriden
S. Adhikari
Sondipon Adhikari
Hamed Haddad Khodaparast
format Journal article
container_title Composite Structures
container_volume 131
container_start_page 594
publishDate 2015
institution Swansea University
issn 0263-8223
doi_str_mv 10.1016/j.compstruct.2015.06.011
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised
document_store_str 1
active_str 0
description This paper presents the quantification of rotational and ply level uncertainty of random natural frequency for laminated composite conical shells by using surrogate modeling approach. The stochastic eigenvalue problem is solved by using QR iteration algorithm. Sensitivity analysis is carried out to address the influence of different input parameters on the output natural frequencies. The sampling size and computational cost is reduced by employing the present approach compared to direct Monte Carlo simulation. The stochastic mode shapes are also depicted for a typical laminate configuration. Statistical analysis is presented to illustrate the results and its performance.
published_date 2015-11-01T12:47:21Z
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score 11.247077

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