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Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation.

Record Type:	Language materials, manuscript : Monograph/item
Title/Author:	Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation./
Author:	Miller, Justin D.
Description:	1 online resource (131 pages)
Notes:	Source: Masters Abstracts International, Volume: 57-01.
Contained By:	Masters Abstracts International57-01(E).
Subject:	Aerospace engineering. -
Online resource:	click for full text (PQDT)
ISBN:	9780355266115

Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation.
Miller, Justin D.

Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation. - 1 online resource (131 pages)

Source: Masters Abstracts International, Volume: 57-01.

Thesis (M.S.A.A.)

Includes bibliographical references

Inexpensive, lightweight, and complex structural components, which are as strong as existing metal components and provide optimal impact performance, are necessary to improve design efficiency. A hybrid approach to composites manufacturing utilizes the structural performance of continuous fiber materials and the design flexibility of discontinuous fiber reinforced thermoplastics.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2018

Mode of access: World Wide Web

ISBN: 9780355266115Subjects--Topical Terms:

686400
Aerospace engineering.
Index Terms--Genre/Form:

554714
Electronic books.

Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation.
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100 1 $a Miller, Justin D. $3 1182980
245 1 0 $a Informing Hybrid-Molded Composite Performance Using Manufacturing Process Simulation.
264 0 $c 2017
300 $a 1 online resource (131 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
500 $a Source: Masters Abstracts International, Volume: 57-01.
500 $a Advisers: R. Byron Pipes; Wenbin Yu.
502 $a Thesis (M.S.A.A.) $c Purdue University $d 2017.
504 $a Includes bibliographical references
520 $a Inexpensive, lightweight, and complex structural components, which are as strong as existing metal components and provide optimal impact performance, are necessary to improve design efficiency. A hybrid approach to composites manufacturing utilizes the structural performance of continuous fiber materials and the design flexibility of discontinuous fiber reinforced thermoplastics.
520 $a Composite performance is dependent on the properties of the constituent materials and the orientation of the reinforcements. The orientation, and thus the performance, of composite reinforcements are determined by the manufacturing process. Accurate modeling of composite performance requires capturing the as-manufactured material properties. Commercial process simulation tools exist for thermoforming of continuous fiber composites as well as molding of discontinuous fiber composites which allow prediction of the as-manufactured fiber orientations. These fiber orientations may be coupled with multi-scale material modeling tools to predict effective properties for use in performance simulations.
520 $a A process has been developed for combining the thermoforming and molding process simulations to inform the performance of hybrid-molded composite materials. These results inform the performance by capturing fiber orientation of each of the materials and predicting as-manufactured effective properties. The dissimilar material properties lead to additional design challenges including the bonding interface and dimensional instability. The combined manufacturing process simulations enable the capture of these properties in performance simulations which will improve the hybrid-molded composite design process.
520 $a Studies on a simple coupon and a generic complex beam demonstrate the effect of including as-manufactured material properties in performance simulations. Other phenomena that must be considered in performance and process design of hybrid-molded composites have been evaluated including dimensional stability, interface temperatures, weld lines, and air traps.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2018
538 $a Mode of access: World Wide Web
650 4 $a Aerospace engineering. $3 686400
655 7 $a Electronic books. $2 local $3 554714
690 $a 0538
710 2 $a ProQuest Information and Learning Co. $3 1178819
710 2 $a Purdue University. $b Aeronautics and Astronautics. $3 845678
773 0 $t Masters Abstracts International $g 57-01(E).
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10608001 $z click for full text (PQDT)