Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body

In this paper, multi-bubble pressure cabin is proposed for the flat fuselage of blended-wing-body(BWB) autonomous underwater vehicle(AUV). It has strong compressive capacity and makes full use of the fuselage space. Radial basis function surrogate model and Kriging surrogate model are used to constr...

Full description

Bibliographic Details
Format: Article
Language:zho
Published: EDP Sciences 2018-08-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p664.pdf
_version_ 1797428290994044928
collection DOAJ
description In this paper, multi-bubble pressure cabin is proposed for the flat fuselage of blended-wing-body(BWB) autonomous underwater vehicle(AUV). It has strong compressive capacity and makes full use of the fuselage space. Radial basis function surrogate model and Kriging surrogate model are used to construct mixture surrogate model for higher accuracy. Two infill sampling methods are adopted:the candidate point sampling and the local optimal sampling. Multi-step optimization of multi-bubble pressure cabin is carried out including shape optimization and structure optimization. To optimize shape, the maximum displacement is selected as the objective function and the shape constraint is chosen as the constraint condition. The minimum structural quality is selected as the objective function, the maximum equivalent stress and bulking factor are chosen as the constraint condition to optimize structure. Finite element method(FEM) analysis is carried out to study the strength and stability performance of multi-bubble pressure cabin using the commercial computational structural mechanics code ANSYS.
first_indexed 2024-03-09T08:56:52Z
format Article
id doaj.art-1bd5ddd8aa524fa2a7862dca6d4338ab
institution Directory Open Access Journal
issn 1000-2758
2609-7125
language zho
last_indexed 2024-03-09T08:56:52Z
publishDate 2018-08-01
publisher EDP Sciences
record_format Article
series Xibei Gongye Daxue Xuebao
spelling doaj.art-1bd5ddd8aa524fa2a7862dca6d4338ab2023-12-02T12:47:37ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252018-08-0136466467010.1051/jnwpu/20183640664jnwpu2018364p664Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body012School of Marine Science and Technology, Northwestern Polytechnical UniversitySchool of Marine Science and Technology, Northwestern Polytechnical UniversitySchool of Marine Science and Technology, Northwestern Polytechnical UniversityIn this paper, multi-bubble pressure cabin is proposed for the flat fuselage of blended-wing-body(BWB) autonomous underwater vehicle(AUV). It has strong compressive capacity and makes full use of the fuselage space. Radial basis function surrogate model and Kriging surrogate model are used to construct mixture surrogate model for higher accuracy. Two infill sampling methods are adopted:the candidate point sampling and the local optimal sampling. Multi-step optimization of multi-bubble pressure cabin is carried out including shape optimization and structure optimization. To optimize shape, the maximum displacement is selected as the objective function and the shape constraint is chosen as the constraint condition. The minimum structural quality is selected as the objective function, the maximum equivalent stress and bulking factor are chosen as the constraint condition to optimize structure. Finite element method(FEM) analysis is carried out to study the strength and stability performance of multi-bubble pressure cabin using the commercial computational structural mechanics code ANSYS.https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p664.pdfmulti-bubble pressure cabinmixture surrogate modelmulti-step optimization designfinite element method
spellingShingle Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
Xibei Gongye Daxue Xuebao
multi-bubble pressure cabin
mixture surrogate model
multi-step optimization design
finite element method
title Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
title_full Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
title_fullStr Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
title_full_unstemmed Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
title_short Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body
title_sort multi step structural optimization design of multi bubble pressure cabin in the autonomous underwater vehicle with blended wing body
topic multi-bubble pressure cabin
mixture surrogate model
multi-step optimization design
finite element method
url https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p664.pdf