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Design Optimisation of a Composite Overwrapped Pressure Vessel through Finite Element Analysis.

Record Type:	Language materials, manuscript : Monograph/item
Title/Author:	Design Optimisation of a Composite Overwrapped Pressure Vessel through Finite Element Analysis./
Author:	Chowdhury, Nahin Bahar.
Description:	1 online resource (62 pages)
Notes:	Source: Masters Abstracts International, Volume: 81-04.
Contained By:	Masters Abstracts International81-04.
Subject:	Mechanical engineering. -
Online resource:	click for full text (PQDT)
ISBN:	9781085689328

Design Optimisation of a Composite Overwrapped Pressure Vessel through Finite Element Analysis.
Chowdhury, Nahin Bahar.

Design Optimisation of a Composite Overwrapped Pressure Vessel through Finite Element Analysis. - 1 online resource (62 pages)

Source: Masters Abstracts International, Volume: 81-04.

Thesis (M.S.)--Texas A&M University - Kingsville, 2018.

Includes bibliographical references

Composite overwrapped pressure vessels (COPVs) are presently utilized at National Aeronautics & Space Administration and other agencies to contain high-pressure fluids in propulsion. These COPV's are used in space shuttles, space stations, aircraft technology, etc. These COPVs have a huge advantage in all kinds of metal vessels; however, when contrasted with every single metal vessel, COPVs require special design criteria, assembling, and test prerequisites. Therefore, design optimization of a filament wound pressure vessel is the main goal of this thesis. Finite element analysis is done on the polymer-lined composite overwrapped pressure vessel (type IV COPV) by numerical methods using Abaqus Wound Composite Modeler to improve the design. In this thesis, change in layer quantities and the winding angle are considered to find out the burst pressure for optimal design parameters of type IV COPV. Tsai Wu, Tsai Hill, maximum strain, maximum stress failure criteria are considered to figure out the burst pressure of the type IV COPV. Numerical simulation results were also compared with the experimental result to validate the numerical results.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9781085689328Subjects--Topical Terms:

557493
Mechanical engineering.
Subjects--Index Terms:

Composite overwrapped pressure vesselsIndex Terms--Genre/Form:

554714
Electronic books.

Design Optimisation of a Composite Overwrapped Pressure Vessel through Finite Element Analysis.
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500 $a Source: Masters Abstracts International, Volume: 81-04.
500 $a Advisor: Alam, Shah.
502 $a Thesis (M.S.)--Texas A&M University - Kingsville, 2018.
504 $a Includes bibliographical references
520 $a Composite overwrapped pressure vessels (COPVs) are presently utilized at National Aeronautics & Space Administration and other agencies to contain high-pressure fluids in propulsion. These COPV's are used in space shuttles, space stations, aircraft technology, etc. These COPVs have a huge advantage in all kinds of metal vessels; however, when contrasted with every single metal vessel, COPVs require special design criteria, assembling, and test prerequisites. Therefore, design optimization of a filament wound pressure vessel is the main goal of this thesis. Finite element analysis is done on the polymer-lined composite overwrapped pressure vessel (type IV COPV) by numerical methods using Abaqus Wound Composite Modeler to improve the design. In this thesis, change in layer quantities and the winding angle are considered to find out the burst pressure for optimal design parameters of type IV COPV. Tsai Wu, Tsai Hill, maximum strain, maximum stress failure criteria are considered to figure out the burst pressure of the type IV COPV. Numerical simulation results were also compared with the experimental result to validate the numerical results.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2024
538 $a Mode of access: World Wide Web
650 4 $a Mechanical engineering. $3 557493
650 4 $a Materials science. $3 557839
653 $a Composite overwrapped pressure vessels
653 $a Filament wound pressure vessel
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