Mechanical Properties Investigation of Composite Material Under Different Parameters Variations

The main objective of this research is to design and select a composite plate to be used in fabricating wing skins of light unman air vehicle (UAV). The mechanical properties, weight and cost are the basis criteria of this selection. The fiber volume fraction, fillers and type of fiber wit...

Descripción completa

Guardado en:

Detalles Bibliográficos
Autor principal:	Farag M. Mohammed
Formato:	article
Lenguaje:	EN
Publicado:	Al-Khwarizmi College of Engineering – University of Baghdad 2017
Materias:	Mechanical properties composite material polyester Taguchi technique Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/17e93a6a7a8f4fbf83b37dddc3134b2d
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

id	oai:doaj.org-article:17e93a6a7a8f4fbf83b37dddc3134b2d
record_format	dspace
spelling	oai:doaj.org-article:17e93a6a7a8f4fbf83b37dddc3134b2d2021-12-02T05:46:59ZMechanical Properties Investigation of Composite Material Under Different Parameters Variations10.22153/kej.2017.09.0011818-11712312-0789https://doaj.org/article/17e93a6a7a8f4fbf83b37dddc3134b2d2017-03-01T00:00:00Zhttp://alkej.uobaghdad.edu.iq/index.php/alkej/article/view/335https://doaj.org/toc/1818-1171https://doaj.org/toc/2312-0789 The main objective of this research is to design and select a composite plate to be used in fabricating wing skins of light unman air vehicle (UAV). The mechanical properties, weight and cost are the basis criteria of this selection. The fiber volume fraction, fillers and type of fiber with three levels for each were considered to optimize the composite plate selection. Finite element method was used to investigate the stress distribution on the wing at cruise flight condition in addition to estimate the maximum stress. An experiments plan has been designed to get the data on the basis of Taguchi technique. The most effective parameters at the process to be find out by employing L9 (33) orthogonal array, signal to noise ratio (S/N), main effect and analysis of variance (ANOVA). The results show that, the experimental and the predicted results are very close. It was found that the type of fiber is the most effective parameter on the plate selection, followed by filler content and then the fiber volume fraction. The best parameters combinations are ((E-glass woven roving + unidirectional carbon) fiber, 7.5% graphite filler and 30% fiber volume fraction). This combination provides good mechanical properties, high safety factor, acceptable cost, and offers weight savings on average by 40% percent as compared to aluminum alloy. Farag M. MohammedAl-Khwarizmi College of Engineering – University of BaghdadarticleMechanical propertiescomposite materialpolyesterTaguchi techniqueChemical engineeringTP155-156Engineering (General). Civil engineering (General)TA1-2040ENAl-Khawarizmi Engineering Journal, Vol 13, Iss 1 (2017)
institution	DOAJ
collection	DOAJ
language	EN
topic	Mechanical properties composite material polyester Taguchi technique Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Mechanical properties composite material polyester Taguchi technique Chemical engineering TP155-156 Engineering (General). Civil engineering (General) TA1-2040 Farag M. Mohammed Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
description	The main objective of this research is to design and select a composite plate to be used in fabricating wing skins of light unman air vehicle (UAV). The mechanical properties, weight and cost are the basis criteria of this selection. The fiber volume fraction, fillers and type of fiber with three levels for each were considered to optimize the composite plate selection. Finite element method was used to investigate the stress distribution on the wing at cruise flight condition in addition to estimate the maximum stress. An experiments plan has been designed to get the data on the basis of Taguchi technique. The most effective parameters at the process to be find out by employing L9 (33) orthogonal array, signal to noise ratio (S/N), main effect and analysis of variance (ANOVA). The results show that, the experimental and the predicted results are very close. It was found that the type of fiber is the most effective parameter on the plate selection, followed by filler content and then the fiber volume fraction. The best parameters combinations are ((E-glass woven roving + unidirectional carbon) fiber, 7.5% graphite filler and 30% fiber volume fraction). This combination provides good mechanical properties, high safety factor, acceptable cost, and offers weight savings on average by 40% percent as compared to aluminum alloy.
format	article
author	Farag M. Mohammed
author_facet	Farag M. Mohammed
author_sort	Farag M. Mohammed
title	Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
title_short	Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
title_full	Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
title_fullStr	Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
title_full_unstemmed	Mechanical Properties Investigation of Composite Material Under Different Parameters Variations
title_sort	mechanical properties investigation of composite material under different parameters variations
publisher	Al-Khwarizmi College of Engineering – University of Baghdad
publishDate	2017
url	https://doaj.org/article/17e93a6a7a8f4fbf83b37dddc3134b2d
work_keys_str_mv	AT faragmmohammed mechanicalpropertiesinvestigationofcompositematerialunderdifferentparametersvariations
_version_	1718400216688754688

Mechanical Properties Investigation of Composite Material Under Different Parameters Variations

Ejemplares similares