國立虎尾科技大學 |

Experimental Characterization and Fracture Behavior of Graphene Nanocomposites.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Experimental Characterization and Fracture Behavior of Graphene Nanocomposites./
作者:	Mefford, Cory Hage.
面頁冊數:	1 online resource (94 pages)
附註:	Source: Masters Abstracts International, Volume: 56-06.
Contained By:	Masters Abstracts International56-06(E).
標題:	Aerospace engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9780355121971

Experimental Characterization and Fracture Behavior of Graphene Nanocomposites.
Mefford, Cory Hage.

Experimental Characterization and Fracture Behavior of Graphene Nanocomposites. - 1 online resource (94 pages)

Source: Masters Abstracts International, Volume: 56-06.

Thesis (Master's)

Includes bibliographical references

This work investigates the structural scaling of polymer/graphene nanocomposites. Fracture tests were conducted on geometrically scaled Single Edge Notch Bending (SENB) specimens with varying contents of graphene. It was shown that while the scaling of the pristine polymer follows Linear Elastic Fracture Mechanics (LEFM), this is not the case for nanocomposites, even for very low graphene contents. In fact, small specimens had a more pronounced ductility with limited scaling and a significant deviation from LEFM whereas larger specimens behaved in a more brittle way, with scaling of nominal strength closer to the one predicted by LEFM. This behavior is due to the significant size of the Fracture Process Zone (FPZ) compared to the specimen size which affects the overall fracturing behavior. This latter aspect needs to be taken into serious consideration since it is shown that, for the specimen sizes investigated in this work, neglecting the non-linear effects of the FPZ can lead to an underestimation of the fracture energy as high as 113%, this error decreasing for increasing specimen sizes. These findings were applied to previously published literature data, where it was shown that most of the specimens tested belonged in the transitional region between ductile and brittle behavior. As a result, the greatest deviation found between LEFM and SEL models was 156%.

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

Mode of access: World Wide Web

ISBN: 9780355121971Subjects--Topical Terms:

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

554714
Electronic books.

Experimental Characterization and Fracture Behavior of Graphene Nanocomposites.
LDR:02672ntm a2200361Ki 4500 001 908700
005 20180330125241.5
006 m o u
007 cr mn||||a|a||
008 190606s2017 xx obm 000 0 eng d
020 $a 9780355121971
035 $a (MiAaPQ)AAI10288801
035 $a (MiAaPQ)washington:17235
035 $a AAI10288801
040 $a MiAaPQ $b eng $c MiAaPQ
099 $a TUL $f hyy $c available through World Wide Web
100 1 $a Mefford, Cory Hage. $3 1178957
245 1 0 $a Experimental Characterization and Fracture Behavior of Graphene Nanocomposites.
264 0 $c 2017
300 $a 1 online resource (94 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: 56-06.
500 $a Adviser: Marco Salviato.
502 $a Thesis (Master's) $c University of Washington $d 2017.
504 $a Includes bibliographical references
520 $a This work investigates the structural scaling of polymer/graphene nanocomposites. Fracture tests were conducted on geometrically scaled Single Edge Notch Bending (SENB) specimens with varying contents of graphene. It was shown that while the scaling of the pristine polymer follows Linear Elastic Fracture Mechanics (LEFM), this is not the case for nanocomposites, even for very low graphene contents. In fact, small specimens had a more pronounced ductility with limited scaling and a significant deviation from LEFM whereas larger specimens behaved in a more brittle way, with scaling of nominal strength closer to the one predicted by LEFM. This behavior is due to the significant size of the Fracture Process Zone (FPZ) compared to the specimen size which affects the overall fracturing behavior. This latter aspect needs to be taken into serious consideration since it is shown that, for the specimen sizes investigated in this work, neglecting the non-linear effects of the FPZ can lead to an underestimation of the fracture energy as high as 113%, this error decreasing for increasing specimen sizes. These findings were applied to previously published literature data, where it was shown that most of the specimens tested belonged in the transitional region between ductile and brittle behavior. As a result, the greatest deviation found between LEFM and SEL models was 156%.
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
650 4 $a Engineering. $3 561152
650 4 $a Mechanical engineering. $3 557493
655 7 $a Electronic books. $2 local $3 554714
690 $a 0538
690 $a 0537
690 $a 0548
710 2 $a ProQuest Information and Learning Co. $3 1178819
710 2 $a University of Washington. $b Aeronautics and Astronautics. $3 1178958
773 0 $t Masters Abstracts International $g 56-06(E).
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10288801 $z click for full text (PQDT)