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02938nam a2200517 i 4500 |
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55919a47-0d1e-4f47-99d5-dcd7f39b4b34 |
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20230617000000.0 |
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160219s1993 pau|||||o|||||||||||eng|| |
| 024 |
7 |
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|a 10.1520/STP24300S
|2 doi
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| 035 |
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|a (IN-ChSCO)ASTMSTP24300S
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| 040 |
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|a ASTM
|c SCOPE
|b eng
|e rda
|d PAU
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| 041 |
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|a eng
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| 100 |
1 |
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|a Harris, CE.,
|e author
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| 245 |
1 |
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|a Translaminate Fracture of Notched Graphite/Epoxy Laminates /
|c CE. Harris, DH. Morris
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| 264 |
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|a West Conshohocken, Pa. :
|b ASTM International,
|c 1993
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| 300 |
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|a 1 online resource (24 pages) :
|b illustrations, figures, tables
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| 336 |
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|a text
|2 rdacontent
|b txt
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| 337 |
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|a computer
|2 rdamedia
|b c
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| 338 |
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|a online resource
|2 rdacarrier
|b cr
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| 347 |
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|a text file
|b PDF
|2 rda
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| 504 |
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|a Includes bibliographical references
|b 16
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| 506 |
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|a Restricted for use by site license.
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| 520 |
3 |
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|a The strength of three notched graphite/epoxy laminates has been shown experimentally to be a function of laminate thickness. The notched strength of the [0/±45/90]ns and [0/90]ns laminates decreased toward asymptotic values with increasing laminate thickness. Conversely, the notched strength of the [0/±45]ns laminate increased toward an asymptotic value with increasing laminate thickness. For all three laminate types, the notched strength decreased with increasing notch size, regardless of thickness. The fracture of the thick laminates were essentially uniform and self-similar with the notch. The "universal" value of the general toughness parameter, Qc/?tuf = 1.5?mm (0.30?in.), developed by Poe successfully predicted the notched strength of the thick laminates. The strength of specimens with surface cuts was predicted using a linear elastic, homogeneous, isotropic fracture mechanics solution
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| 541 |
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|a ASTM International
|3 PDF
|c Purchase price
|h USD25
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| 588 |
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|a Description based on publisher's website, viewed February 19, 2016
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| 650 |
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0 |
|a Composite materials
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| 650 |
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|a Fatigue (materials)
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| 650 |
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0 |
|a Fracture mechanics
|v Congresses
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| 650 |
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|a Fracture mechanics
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| 650 |
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|a Fracture toughness
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| 650 |
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|a Fracture
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| 650 |
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|a Notched laminates
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| 650 |
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0 |
|a Thick laminates
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| 650 |
1 |
4 |
|a Notched laminates
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| 650 |
2 |
4 |
|a Composite materials
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| 650 |
2 |
4 |
|a Fatigue (materials)
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| 650 |
2 |
4 |
|a Fracture mechanics
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| 650 |
2 |
4 |
|a Fracture toughness
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| 650 |
2 |
4 |
|a Fracture
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| 650 |
2 |
4 |
|a Thick laminates
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| 700 |
1 |
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|a Morris, DH.,
|e author
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| 710 |
2 |
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|a ASTM International
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| 710 |
2 |
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|a American Society for Testing and Materials
|t Selected Technical Papers.
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| 710 |
2 |
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|a American Society for Testing and Materials
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| 740 |
0 |
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|a ASTM digital library
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| 999 |
1 |
0 |
|i 55919a47-0d1e-4f47-99d5-dcd7f39b4b34
|l 9978998709803681
|s US-PU
|m translaminate_fracture_of_notched_graphite_epoxy_laminates_________________1993_______astmia________________________________________harris__ce_________________________e
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